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Structural Analysis of a vault of the Administration building of the Hospital Sant Pau Erasmus Mundus Programme ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS i DECLARATION Name: Juan C. Arias Email: [email protected] Title of the Msc Dissertation: Structural Analysis of a vault of the Administration building of the Hospital Sant Pau Supervisor: Pere Roca i Fabregat Year: 2013 I hereby declare that all information in this document has been obtained and presented in accordance with academic rules and ethical conduct. I also declare that, as required by these rules and conduct, I have fully cited and referenced all material and results that are not original to this work. I hereby declare that the MSc Consortium responsible for the Advanced Masters in Structural Analysis of Monuments and Historical Constructions is allowed to store and make available electronically the present MSc Dissertation. University: Universitat Politècnica de Catalunya - UPC Date: July 9 of 2013 Signature:

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Page 1: Juan Arias - 07.13.13 v2

Structural Analysis of a vault of the Administration building of the Hospital Sant Pau

Erasmus Mundus Programme

ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS i

DECLARATION

Name: Juan C. Arias

Email: [email protected]

Title of the

Msc Dissertation:

Structural Analysis of a vault of the Administration building of the Hospital

Sant Pau

Supervisor: Pere Roca i Fabregat

Year: 2013

I hereby declare that all information in this document has been obtained and presented in accordance

with academic rules and ethical conduct. I also declare that, as required by these rules and conduct, I

have fully cited and referenced all material and results that are not original to this work.

I hereby declare that the MSc Consortium responsible for the Advanced Masters in Structural Analysis

of Monuments and Historical Constructions is allowed to store and make available electronically the

present MSc Dissertation.

University: Universitat Politècnica de Catalunya - UPC

Date: July 9 of 2013

Signature:

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ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS iii

A mi familia:

A mi padre, fuente de Ejemplo y Sabiduría

A mi madre, fuente de Amor y mi guía

A mi hermano, mi gran amigo

A mi hermana, por toda su felicidad y alegría

Al perro, por ser tan inquieto

Gracias a la vida, por habernos juntado

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ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS v

ACKNOWLEDGEMENTS

I would like to thank Pere Roca for giving me the opportunity to work on this amazing building, for

allow me to learn more about timbrel constructions, for his invaluable support and for all his

recommendations about the model.

I am sincerely grateful with Yohei Endo, for his help and advises about using DIANA, for the time he

spent giving me advises, for all the questions answered, even when I made the same question several

times.

My most especial acknowledgement to Salvador Tarragó for introducing me the constructions without

centering -being the timbrel vaults one example- and, most important, for guiding and helping me to

improve myself as human being.

I will also like to thanks to Francisco, “mi chucha po”, for his invaluable friendship and for being my

support during all the time I spent in Europe... “gracias mi hermano”.

Many thanks to my roommates and all the friends I made in Padova and Barcelona, especially Adeliya

for being so kind with me. I really had a good time and I will never forget any of you.

Thanks to my aunts and my grandmother for their moral support, to my professors in Colombia,

especially Maria del Pilar Duque and Maria del Pilar Arroyave, and to all my friends there for not

forgetting about me.

Finalmente, a mi familia, que han sido mi principal apoyo y soporte durante toda mi vida; por más

palabras que escriba, siempre quedaré corto en agradecimientos por todo lo que han hecho por mi,

los quiero mucho.

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ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS vii

ABSTRACT

Structural Analysis of a vault of the Administratio n building of the Hospital Sant Pau

The main goal of this thesis is to assess the load-carrying capacity of one of the vaults located on the

Administration Building of the Hospital Sant Pau, a UNESCO World Heritage site located in Barcelona,

Spain. Firstly, a brief historical survey of the city and the complex is done, in order to understand the

hospital complex’s own cultural, social and environmental values. Also, an introduction to timbrel

construction -the constructive technique used for building all the hospital vaults- is detailed, explaining

the execution process and the historical development, reviewing the state of the art on timbrel

construction analysis and describing the most common timbrel vault typologies built. The main

available methods for studying masonry historical constructions are detailed, an introduction to the

history of shell structures analysis is provided and some of the most recent studies regarding timbrel

constructions analysis are presented.

Secondly, the main characteristics of the numerical model are covered, like the mesh generated, type

of elements used, integration schemes, material modelling and iterative procedure implemented.

Then, the numerical model development process is explained, till a satisfactory representation of the

real structure is achieved. By this, the load-carrying capacity of the vault is assessed. In addition, a

brief parametrical analysis varying the values of compression strength and fracture energy is provided.

Finally, some conclusions and recommendations for future analysis are given.

The results of the study constitute an important support to the structural assessment of the building

and can contribute to the evaluation of further studies or possible interventions.

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RESUMEN

Análisis estructural de una de las bóvedas del edif icio de la Administración del Hospital

Sant Pau.

La principal finalidad de este trabajo es evaluar la capacidad de carga de una de las bóvedas del

edificio de la Administración del Hospital Sant Pau, un complejo declarado Patrimonio de la

Humanidad por la UNESCO, ubicado en la ciudad de Barcelona, España. Para esto, se realizó

inicialmente un corto repaso histórico de la ciudad y del complejo hospitalario con el fin de entender

sus valores culturales, sociales y ambientales. Además, se hace una introducción al sistema de

construcción tabicada (la técnica constructiva utilizada para la construcción de las bóvedas del

hospital), una explicación del modo de ejecución y del desarrollo histórico, un resumen del estado del

arte sobre el cálculo estructural de bóvedas tabicadas y una descripción de las tipologías más

comunes de bóvedas tabicadas. Los principales métodos para el estudio de edificios históricos de

fábrica son expuestos, se presenta una introducción al análisis estructural de cáscaras así como los

últimos estudios realizados sobre análisis de estructuras tabicadas.

Posteriormente, son explicadas las principales características del modelo numérico como son la malla

generada, tipos de elementos, esquemas de integración, modelado del material y procesos de

iteración implementados. Así mismo, se describe el proceso de desarrollo del modelo numérico hasta

que se obtiene una representación satisfactoria de la estructural real. Con esto, la capacidad de carga

del modelo es evaluada. Adicionalmente, un pequeño estudio paramétrico es llevado a cabo,

haciendo variar los valores de resistencia a la compresión y energía de fractura. Finalmente, se dan

algunas conclusiones y recomendaciones para futuros análisis de este tipo.

Los resultados de este estudio constituyen un importante soporte para la evaluación estructural del

edificio y pueden contribuir a la evaluación de futuros estudios o posibles intervenciones.

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RESUM

Anàlisi estructural d'una de les voltes de l'edific i de l'Administració de l'Hospital Sant Pau.

La principal finalitat d'aquest treball és avaluar la capacitat de càrrega d'una de les voltes de l'edifici

de l'Administració de l'Hospital Sant Pau, un complex declarat Patrimoni de la Humanitat per la

UNESCO ubicat a la ciutat de Barcelona, Espanya. Per fer-ho, es va realitzar inicialment un curt repàs

històric de la ciutat i del complex hospitalari per poder entendre els seus valors culturals, socials i

ambientals. A més a més, es fa una introducció al sistema de construcció maó de pla (la tècnica

constructiva utilitzada per a la construcció de les voltes de l'hospital), una explicació de la manera

d'execució i del desenvolupament històric, un resum de l'estat de l'art sobre el càlcul estructural de

voltes de maó de pla i una descripció de les tipologies més comuns de voltes de maó de pla. Els

principals mètodes per a l'estudi d'edificis històrics de fàbrica són exposats, es presenta una

introducció a l'anàlisi estructural de closca i els últims estudis realitzats sobre anàlisi d'estructures de

maó de pla.

Posteriorment, són explicades les principals característiques del model numèric com ara la malla

generada, tipus d'elements, esquemes d'integració, modelatge del material i processos d'iteració

implementats. Així mateix, es descriu el procés de desenvolupament del model numèric fins que

s'obté una representació satisfactòria de l'estructural real. Amb això, la capacitat de càrrega del model

és avaluada. Addicionalment, un petit estudi paramètric és dut a terme, fent variar els valors de

resistència a la compressió i energia de fractura. Finalment, es proposen algunes conclusions i

recomanacions per a futures anàlisis semblants a la d’aquesta avaluació.

Els resultats d'aquest estudi constitueixen un important suport per a l'avaluació estructural de l'edifici i

poden contribuir a l'avaluació de futurs estudis o possibles intervencions.

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RÉSUMÉ

´

Analyse structurelle d’une voûte du bâtiment admini stratif de l'Hôpital Sant Pau

Le but principal de cette thèse est d'évaluer la capacité portante d'une des voûtes du bâtiment

administratif de l'Hôpital Sant Pau, un site classé patrimoine mondial de l'UNESCO et situé à

Barcelone en Espagne. Tout d'abord, une rapide recherche historique sur la ville et sur le complexe

est menée à bien afin de comprendre les valeurs culturelles, sociales et environnementales du

complexe hospitalier. Ensuite est présentée une introduction à la construction des voûtes dites

catalanes – technique constructive employée pour l’ensemble des voûtes de l’hôpital. Dans cette

partie le processus d’exécution, le développement historique ainsi que l’état de l’art de l’analyse de ce

type de construction sont notamment abordés. D’autre part une description des principales typologies

de voûtes catalanes est donnée. En outre, les principales méthodes disponibles pour l'étude des

constructions historiques en maçonnerie sont exposées, une introduction à l'histoire de l'analyse des

structures en coque est fournie et enfin quelques-unes des plus récentes études concernant l'analyse

des constructions avec voûtes catalanes est présentée.

Dans un deuxième temps les principales caractéristiques du modèle numérique sont données, comme

par exemple la génération du maillage, le type d’éléments utilisés, les systèmes d'intégration, la

modélisation des matériaux ainsi que la procédure d’itération mise en œuvre. Ensuite, le processus

d'élaboration du modèle numérique permettant d’obtenir une représentation satisfaisante de la

structure réelle est expliqué. Ce modèle est par la suite utilisé pour évaluer la capacité portante de la

voûte. En outre, une brève analyse paramétrique basée sur les valeurs de résistance à la

compression et sur les valeurs de l’énergie de rupture est fournie. Enfin, sont données les principales

conclusions et recommandations pour de futures analyses.

Les résultats de la présente étude constituent un soutien important dans l'évaluation de la structure du

bâtiment et pourront contribuer à l'évaluation de nouvelles études ou à de possibles interventions

.

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TABLE OF CONTENTS

1 Introduction ..................................................................................................................... 1

1.1 Objectives ................................................................................................................ 1

1.1.1 General ............................................................................................................. 1

1.1.2 Specific ............................................................................................................. 1

1.2 Thesis organization .................................................................................................. 1

2 Hospital Sant Pau ........................................................................................................... 3

2.1 Geographic location ................................................................................................. 3

2.1.1 The City: Barcelona .......................................................................................... 3

2.1.2 Urban emplacement ......................................................................................... 4

2.2 History ..................................................................................................................... 5

2.3 The Administration Building ..................................................................................... 6

2.3.1 Architectural description ................................................................................... 6

2.3.2 Structural System ............................................................................................. 9

3 Timbrel Vaults ............................................................................................................... 13

3.1 Description ............................................................................................................ 13

3.2 History of timbrel vaults ......................................................................................... 14

3.3 State of the art in timbrel vaults structural analysis ................................................ 19

3.4 Timbrel vault typologies ......................................................................................... 25

3.4.1 Barrel Vault ..................................................................................................... 25

3.4.2 Cross vault ..................................................................................................... 28

3.4.3 Cloister vaults ................................................................................................. 30

3.4.4 “Quatre punts” vault ........................................................................................ 31

3.4.5 Stairs vault ...................................................................................................... 32

4 Structural Analysis of Historical Constructions: Advanced Approaches ......................... 35

4.1 History and challenges .......................................................................................... 35

4.2 Types of modelling ................................................................................................. 37

4.2.1 Elastic Linear Analysis .................................................................................... 37

4.2.2 FEM based approaches. Macro-Modelling ...................................................... 38

4.2.3 FEM based approaches. Discontinuous Models ............................................. 38

4.2.4 FEM based approaches. Micro-Modelling ....................................................... 38

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4.3 Shell structures ...................................................................................................... 39

4.3.1 Introduction to shell structures Elastic Theories development ......................... 39

4.3.2 Advanced approaches: shell historical constructions ...................................... 40

4.3.3 Advanced approaches: timbrel constructions modelling .................................. 41

5 Finite Element Model .................................................................................................... 43

5.1 Software ................................................................................................................ 43

5.2 Geometry ............................................................................................................... 43

5.3 Mesh Generation ................................................................................................... 43

5.4 Element Types ....................................................................................................... 44

5.5 Integration Schemes .............................................................................................. 46

5.6 Material Modelling .................................................................................................. 47

5.6.1 Tensile Craking ............................................................................................... 47

5.6.2 Compressive Behaviour .................................................................................. 47

5.7 Iterative Procedure ................................................................................................ 48

6 Model Development Process ........................................................................................ 49

6.1 Vault Description .................................................................................................... 49

6.1.1 Geometry ........................................................................................................ 49

6.1.2 Mechanical properties ..................................................................................... 51

6.2 Model 1 .................................................................................................................. 51

6.2.1 Model Description ........................................................................................... 51

6.2.2 Results ........................................................................................................... 52

6.3 Model 2 .................................................................................................................. 55

6.3.1 Model Description ........................................................................................... 55

6.3.2 Results ........................................................................................................... 56

6.4 Model 3 .................................................................................................................. 59

6.4.1 Model Description ........................................................................................... 59

6.4.2 Results ........................................................................................................... 60

6.5 Model 4 .................................................................................................................. 63

6.5.1 Model Description ........................................................................................... 63

6.5.2 Results ........................................................................................................... 64

6.6 Model 5 .................................................................................................................. 67

6.6.1 Model Description ........................................................................................... 67

6.6.2 Results ........................................................................................................... 68

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6.7 Model 6 .................................................................................................................. 71

6.7.1 Model Description ........................................................................................... 71

6.7.2 Results ........................................................................................................... 72

6.8 Model 7 .................................................................................................................. 76

6.8.1 Model Description ........................................................................................... 76

6.8.2 Results ........................................................................................................... 77

6.9 Model 8 .................................................................................................................. 80

6.9.1 Model Description ........................................................................................... 80

6.9.2 Results ........................................................................................................... 81

6.10 Model Comparison ................................................................................................. 86

7 Parametrical analysis .................................................................................................... 89

7.1 Compressive strength ............................................................................................ 89

7.1.1 fc = 1 MPa ....................................................................................................... 89

7.1.2 fc = 2 MPa ....................................................................................................... 91

7.1.3 Compressive strength comparison .................................................................. 92

7.2 Fracture Energy ..................................................................................................... 93

7.2.1 Gf = 25 N/m .................................................................................................... 93

7.2.2 Gf = 100 N/m .................................................................................................. 94

7.2.3 Fracture energy comparison ........................................................................... 95

8 Conclusions .................................................................................................................. 97

References ......................................................................................................................... .99

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List of Figures

Figure 2.1 - 3D of Hospital Sant Pau .................................................................................. 3

Figure 2.2 - Location of Barcelona ...................................................................................... 3

Figure 2.3 - L'Eixmaple (Museum of History of Barcelona) ................................................. 4

Figure 2.4 - Aerial view of the Hospital de Sant Pau complex ............................................ 5

Figure 2.5 - Original project of the Hospital Sant Pau complex designed by Domènech i

Montaner ........................................................................................................................... 6

Figure 2.6 - Administration Building .................................................................................... 7

Figure 2.7 - Division of the Administration building ............................................................ 7

Figure 2.8 - Lobby .............................................................................................................. 8

Figure 2.9 - Vault case of study .......................................................................................... 9

Figure 2.10 - Vault pendentive arches ................................................................................ 9

Figure 2.11 - Structural system of the basement.. ............................................................ 10

Figure 2.12 - 3D of the Administration Building structure. 10

Figure 2.13 – Metallic structure ........................................................................................ 11

Figure 3.1- Stair Timbrel vault ......................................................................................... 13

Figure 3.2 - Use of tiles for concrete vault constructions by Romans ................................ 14

Figure 3.3 - Timbrel vault proposed by the earl d'Espie .................................................... 15

Figure 3.4 - Advertise drawing showing the largest constructions built by the Gustavino

company ......................................................................................................................... 16

Figure 3.5 - Timbrel vaults construction by (a) Lluis Muncunill and (b) Cesar Martinell ..... 16

Figure 3.6 - Crypta Guell church timbrel vautls, (a) in the interior, (b) at the exterior

portico.................................................................................................................................17

Figure 3.7 - Dome in the Gijón University by Luis Moya .................................................. 17

Figure 3.8 - Le Cobusier, (a) drawings: Sagrada Familia School (b) plans of Sarabhai

House .............................................................................................................................. 18

Figure 3.9 - Eladio Dieste works ....................................................................................... 18

Figure 3.10 - Mapungubwe Interpretation Centre ............................................................. 19

Figure 3.11 – Church project from treatise of Fray Lorenzo de San Nicolás ..................... 19

Figure 3.12 - Load test carried by Guastavino on 1901 ................................................... 21

Figure 3.13 - Guastavino Moreno Espósito drawings: (a) Static graphic analysis for the

Saint John Divine Dome, (b) patent for reinforcement of tension zones in domes ............ 22

Figure 3.14 - Reproduction of Gaudí hanging model ....................................................... 23

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Figure 3.15 - Relationship between the compression equilibrium shape, the thrust network,

its planar projection and the reciprocal diagram, used for applying the TNA method. ....... 25

Figure 3.16 – Wall cavities for supporting the vault ........................................................... 26

Figure 3.17 - Use of strings and light trusses for the construction of a barrel vault . ......... 26

Figure 3.18 – Bondig types. .............................................................................................. 27

Figure 3.19 - Ribs on barrel vaults surface. ...................................................................... 27

Figure 3.20 - Possible deformation by buckling ................................................................ 27

Figure 3.21 - Timbrel cross vault building processes . ...................................................... 28

Figure 3.22 - Cross vault construction process. ................................................................ 29

Figure 3.23 - Constructive process: (a) layers setting, (b) Arrise formation. ...................... 30

Figure 3.24 - Timbrel Cloister vault construction process . ............................................... 31

Figure 3.25 - Timbrel "quatre punts" vault construction process. ...................................... 32

Figure 3.26 – Timbrel stairs vault longitudinal section. ...................................................... 33

Figure 3.27 - Timbrel stair vault directrix drawing. ............................................................ 33

Figure 3.28 - Use of the wood veneer for drawing the generatrix ...................................... 34

Figure 3.29 – Support of a timbrel stair vault over an existing one. ................................... 34

Figure 4.1 – Mexico City Cathedral FEM ......................................................................... 36

Figure 4.2 - Linear elastic analysis of the Güell Colony Crypt ........................................... 37

Figure 4.3 - Discontinuos model ....................................................................................... 38

Figure 4.4 - Modelling strategies . .................................................................................... 39

Figure 4.5 - Study of Saint Marco’s domes in Venice ....................................................... 40

Figure 4.6 - Timbrel dome FEM ....................................................................................... 41

Figure 4.7 - Timbrel dome FEM with (a) shell elements, (b) solid elements . .................... 42

Figure 4.8 - Timbrel dome FEM ....................................................................................... 42

Figure 5.1 - Vault geometry: (a) scheme of lines by TOYSER S.A. (b) generated on

Rhinoceros ....................................................................................................................... 43

Figure 5.2 - Model Meshes: (a) vault (b) vault and walls ................................................... 44

Figure 5.3 - Quadrilateral curved shell element . .............................................................. 45

Figure 5.4 - QU8-CQ40S curved shell elements and thier DOF . ...................................... 45

Figure 5.5 - Beam element . ............................................................................................. 45

Figure 5.6 - BE2-L13B beam elements and its DOF . ....................................................... 46

Figure 5.7 – Triangular curved shell element . .................................................................. 46

Figure 5.8 - Integration scheme for (a) quadrilateral shell elements, (b) triangular shell

elements. .......................................................................................................................... 46

Figure 5.9 – Rankine failure criteria in a two-dimensional stress state.. ............................ 47

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Figure 5.10 - Tension in softening model .......................................................................... 47

Figure 5.11 - Mohr-Coulomb and Drucker-Prager yield condition. .................................... 48

Figure 5.12 - Secant iteration . ......................................................................................... 48

Figure 6.1 - Hospital Sant Pau: location of the vault case of study ................................... 49

Figure 6.2 - Vault plan ...................................................................................................... 50

Figure 6.3 - Model steel elements cross section (IPN-100) ............................................... 50

Figure 6.4 - Model 1: Boundary Conditions ...................................................................... 52

Figure 6.5 - (a) vertical deflection, (b) Total deformed variation ........................................ 52

Figure 6.6 – Load-Displacement curve on the middle of the vault. .................................... 53

Figure 6.7 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface ................ 53

Figure 6.8 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface. .................. 54

Figure 6.9 - Crack Distribution (a) Top Surface, (b) Bottom Surface ................................ 54

Figure 6.10 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface . ............. 55

Figure 6.11 - Model 2: Boundary Conditions..................................................................... 55

Figure 6.12- (a) vertical displacements, (b) Total deformed variation (amplified), (c) Total

deformed shape (amplified) .............................................................................................. 56

Figure 6.13 – Load-Displacement curve on the middle of the vault. .................................. 56

Figure 6.14 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface. ............. 57

Figure 6.15 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface. ................ 58

Figure 6.16 - Crack Distribution (a) Top Surface, (b) Bottom Surface. .............................. 58

Figure 6.17 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface. .............. 58

Figure 6.18 - Proportional steel cross-section ................................................................... 59

Figure 6.19 - Model 3: Boundary Conditions..................................................................... 60

Figure 6.20- (a) vertical displacements, (b) Total deformed variation (amplified), (c) Total

deformed shape (amplified) .............................................................................................. 60

Figure 6.21 - Load-Displacement curve on the middle of the vault. .................................. 61

Figure 6.22 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface. ............. 62

Figure 6.23 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface . ............... 62

Figure 6.24 - Crack Distribution (a) Top Surface, (b) Bottom Surface ............................... 63

Figure 6.25 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface . ............. 63

Figure 6.26 - Model 4: Boundary Conditions..................................................................... 64

Figure 6.27 - (a) vertical displacements, (b) Total deformed variation (amplified) ............. 64

Figure 6.28 - Load-Displacement curve on the middle of the vault. .................................. 65

Figure 6.29 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface . ............ 66

Figure 6.30 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface . ............... 66

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Figure 6.31 - Crack Distribution (a) Top Surface, (b) Bottom Surface .............................. 66

Figure 6.32 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface .............. 67

Figure 6.33 - Model 5: Boundary Conditions ..................................................................... 67

Figure 6.34 - (a) vertical displacements, (b) Total deformed variation (amplified) ............. 68

Figure 6.35 – Load-Displacement curve at the middle of the vault as a factor of self weight.

68

Figure 6.36 – Load-Displacement curve on the middle of the vault. .................................. 69

Figure 6.37 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface. ............. 69

Figure 6.38 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface . ............... 70

Figure 6.39 - Crack Distribution (a) Top Surface, (b) Bottom Surface. .............................. 70

Figure 6.40 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface . ............. 71

Figure 6.41 – Model 6: Boundary Conditions .................................................................... 72

Figure 6.42 - (a) vertical displacements, (b) Total deformed variation (amplified) ............. 72

Figure 6.43 – Load-Displacement curve on the middle of the vault as a factor of self

weight. .............................................................................................................................. 73

Figure 6.44 – Load-Displacement curve on the middle of the vault. .................................. 73

Figure 6.45 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface . ............ 74

Figure 6.46 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface . ............... 74

Figure 6.47 - Crack Distribution (a) Top Surface, (b) Bottom Surface . ............................. 75

Figure 6.48 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface . ............. 75

Figure 6.49 – (a) Ribs, (b) Model 7: Boundary Conditions. ............................................... 76

Figure 6.50 - (a) vertical displacements, (b) Total deformed variation (amplified) ............. 77

Figure 6.51 – Load-Displacement curve at the middle of the vault as a factor of self

weight..................................................................................................................................77

Figure 6.52 – Load-Displacement curve at the middle of the vault. ................................... 78

Figure 6.53 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface. ............. 79

Figure 6.54 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface. ................ 79

Figure 6.55 - Crack Distribution (a) Top Surface, (b) Bottom Surface. .............................. 80

Figure 6.56 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface. .............. 80

Figure 6.57 - Metallic structure (a) existing [González et. al., 2011], (b) Model

simplification. .................................................................................................................... 81

Figure 6.58 - Model 8: Boundary Conditions ..................................................................... 81

Figure 6.59 - (a) vertical displacements, (b) Total deformed variation (amplified) ............. 82

Figure 6.60 - Capacity curve at the middle of the vault as a factor of self weight. ............. 82

Figure 6.61 - Capacity curve at the middle of the vault. .................................................... 83

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Figure 6.62 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface. ............. 84

Figure 6.63 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface. ................ 84

Figure 6.64 - Crack Distribution (a) Top Surface, (b) Bottom Surface. .............................. 85

Figure 6.65 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface . ............. 85

Figure 6.66 – Load-Displacement curve on the middle of the vault as a factor of self weight

for all models. ................................................................................................................... 86

Figure 6.67 – Load-Displacement curve at the middle of the vault for the models. ........... 87

Figure 7.1 – Load-Displacement curve at the middle of the vault for fc = 1 MPa ............... 89

Figure 7.2 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface. ............... 90

Figure 7.3 - Minimum Principal Stresses (a) Top Surface, (b) Bottom Surface. ................ 90

Figure 7.4 – Crack Distribution (a) Top Surface, (b) Bottom Surface. ............................... 90

Figure 7.5 – Load-Displacement curve on the middle of the vault for fc = 2 MPa .............. 91

Figure 7.6 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface . .............. 91

Figure 7.7 - Minimum Principal Stresses (a) Top Surface, (b) Bottom Surface. ................ 92

Figure 7.8 - Compressive strength load-displacement curve comparison ......................... 92

Figure 7.9 – Load-Displacement curve on the middle of the vault for Gf = 25 N/m ........... 93

Figure 7.10 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface. ............. 94

Figure 7.11 – Load-Displacement curve on the middle of the vault for Gf = 100 N/m ....... 94

Figure 7.12 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface. ............. 95

Figure 7.13 – Fracture Energy load-displacement curve comparison ............................... 95

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List of Tables

Table 3-1 – Recommendations of Fray Lorenzo for the dimensions of the abutments in

function of the span ............................................................................................................. 20

Table 6-1 - Tile mechanical properties values ...................................................................... 51

Table 6-2 - Steel mechanical properties values .................................................................... 51

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1 INTRODUCTION

The dissertation has the purpose of analyzing the structural behaviour of one of the vaults of the

Administration Building of the Hospital Sant Pau, a UNESCO World Heritage site located in Barcelona

(Spain). The vaults of this building were built using a traditional constructive technique developed on

the Mediterranean region that reached its maximum architectonical expression during the Catalan

modernism.

The main goal of this thesis is to assess the load-carrying capacity of a vault by a numerical model. It

will also be studied the influence of a number of material mechanical properties in the structural

behaviour of the vault through a parametric investigation conducted using structural analysis software.

The results of the study constitute an important contribution to the structural assessment of the

building and can contribute to the evaluation of further studies or possible interventions.

1.1 Objectives

1.1.1 General

• Develop a numerical model that represents the structural behaviour of one of the vaults

located on the Administration Building of the Hosptial Sant Pau.

1.1.2 Specific

• Provide information about the state of the art regarding timbrel vault constructions by literature

research.

• Recognize the main aspects of the constructive technique employed for timbrel vault

constructions.

• Examine the structural characteristics of the vault; identify the failure mechanism and its

behaviour when submitted to an incremental distributed load.

• Perform a parametric analysis to evaluate the sensibility of the model when some mechanical

properties are changed.

1.2 Thesis organization

On this chapter, there are presented the objectives of this thesis.

Chapter 2 has a brief historical survey of the city and the complex in order to understand the

significance and value of the studied building in relation to the hospital complex own cultural, social

and environmental values, as it is recommended by ICOMOS. Then, the Administration Building is

introduced: a brief geometrical description and an analysis of the structural system is provided.

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Chapter 3 introduces the timbrel construction technique, with a description of its execution, an

historical development, a review of timbrel vault structural analysis state of the art and a summary the

most common timbrel vault typologies built.

Chapter 4 reviews the methods applicable to the study of masonry historical constructions but mainly

focussed on the advanced ones, being numerated firstly the main challenges posed by historical

constructions. After this, a brief history of shell structures analysis is provided to finally focus on the

most recent studies regarding timbrel constructions analysis.

Chapter 5 describes the main aspects of the FE model like the mesh generated, type of elements,

integration schemes, material modelling and iterative procedure.

Chapter 6 contains the model development process till one with satisfactory results is achieved.

Chapter 7 provides a brief parametrical analysis, varying the values of compression strength and

fracture energy.

Chapter 8 includes the conclusions and some recommendations for future analysis.

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2 HOSPITAL SANT PAU

2.1 Geographic location

The Hospital de la Santa Creu i Sant Pau is located in Barcelona, Spain (Figure 2.1). In the present,

restoration works are carried to host international institutions like the University of the United Nations

(UNU), Casa Asia, the European Forest Institute (EFI), the Global Water Operators’ Partnerships

Alliance (GWOPA), etc.

Figure 2.1 - 3D of Hospital Sant Pau (http://desantacreuasantpau.blogspot.com/, 18.06.13)

2.1.1 The City: Barcelona

Figure 2.2 - Location of Barcelona(http://luar-

negeri.kompasiana.com. 18.06.13)

Barcelona is located at the North east of Spain, is the

capital of the province of the same name and of

Catalunya (Figure 2.2). It is on the shores of the

Mediterranean Sea, 120 km from the Pyrenees

mountain range and the border with France. It is limited

in the east by the sea, the Sierra de Collserola on the

west, the Llobregat River on the south and the Besós

River on the north.

The city has hosted many important world events that have contributed to configure the morphology

and have helped to give it an international recognition, being the most relevant the World’s Fair on

1888, the International Exposition on 1929, the Olympic Games on 1992 and the Universal Forum of

Cultures on 2004.

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The first human traces found in the area of the city, are dated back to the late Neolithic period (2000 –

15000 AD). However, the first important settlements will not appear until the centuries VII-VII BC with

the establishment of the Laietanos, an Iberian village. Barcino was the name given by Romans after

the foundation of the city between the years 15-10 BC, being only a small village with 10 hectare and

10.000 habitants. During medieval times it was an important trade centre in the Mediterranean and an

important capital, exercising control over various territories conquered.

After the political and economic splendour during medieval times, it came a darker period after the

War of Succession (1714), in which a great part of the city was destroyed. It will not be until the end of

the XVIII century and the beginning of the XIX that an economical and industrial arise will occur again,

development promoted by a new bourgeois class emerging. This growth will make the city to expand:

the old walls of the city were demolished and a new urban plan of the city –the Eixample, designed by

the engineer Ildefons Cerdá- is implemented (Figure 2.3). The urban plan is characterized by the

network of streets parallel to the sea, crossed by others at right angles, delimitating blocks with

chamfered corners. During this period culture experiments a major revitalization, Catalan language

resurges at a literary level, and Modernism becomes the most important artistic expression of the new

society of Barcelona.

Figure 2.3 - L'Eixmaple (Museum of History of Barcelona)

The city will also experience a great urban transformation on the occasion of the Olympic Games on

1992, the Universal Forum of Cultures on 1994, regenerating the city as it was foreseen by Cerdá on

his urban project. Today, Barcelona is recognized as a “global city” for its cultural, financial, commerce

and tourism, and is one of the most important cities in the Mediterranean Sea.

2.1.2 Urban emplacement

The Hospital Sant Pau is a Modernism complex projected by Lluís Domènech i Montaner, one of the

most important Modernists architects. Placed on nine Cerdá blocks, the complex was set as a series

of isolated pavilions surrounded by gardens and connected by underground tunnels (Figure 2.4).

There were projected 48 independent pavilions, but only 19 were constructed.

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Located on the Horta-Guinardó neighbourhood, is limited by the streets Ronda del Guinardo, carrer

de Sant Quintí, carrer de Sant Antoni i Maria Claret and Carrer de Cartagena. It is also communicated

with the Sagrada Familia by the pedestrian street Avinguda de Gaudí.

Figure 2.4 - Aerial view of the Hospital de Sant Pau complex (Google Earth, 18.06.13)

2.2 History

At the end of the XIX century, a banker named Pau Gil -the son of a Catalan bourgeois family- dies,

destining part of his will for the construction of a hospital in Barcelona. The project was commissioned

to architect Lluis Domènech i Muntaner, who inspired in the design of the best hospitals in Europe: a

hospital centralized in one building or separated in different pavilions. The hospital was designed to

provide all services within and thus isolate it from the city, and in the design project there can be seen

streets, gardens, water supply buildings, a church and even a convent (Figure 2.5).

The complex was projected on 1901, but the construction begun on August 1902 with the earthmoving

works that were extended till June 1904. It was constructed in two phases: the first one, guided by

Domènech between the years 1902 and 1913, constructing 13 modernists buildings while the second,

from 1920, was guided by his son, Pere Domènech i Roura, where another six buildings where

constructed in a more moderate Modernist style, but only four of them following the original project. At

the end of the 1928, the design of Domènech was already abandoned, and the following buildings

erected did not have into account his plan (Figure 2.5).

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On 2003, the construction works of a new building were initiated on the extreme north of the complex

emplacement, with the purpose of substituting progressively all the services located on the old

pavilions. Although the original project was not finished, the complex was declared as World Heritage

Site by the UNESCO on 1997.

Figure 2.5 - Original project of the Hospital Sant Pau complex designed by Domènech i Montaner (http://desantacreuasantpau.blogspot.com/, 18.06.03)

2.3 The Administration Building

2.3.1 Architectural description

The Administration building is a symmetric construction with V shape, delimiting the access to the

hospital complex. It can be subdivided in 5 modules, each of them separated by bearing walls. They

are (Figure 2.6 and Figure 2.7):

1) Central body

2) West body

3) Extreme west body

4) East body

5) Extreme east body

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Figure 2.6 - Administration Building (http://www.eseficiencia.es/, 18.06.13)

Figure 2.7 - Division of the Administration building [BOMA, 2007].

• Central body

Is the part of the building that has the most representative elements and spaces (Figure 2.8). It

contains the entrance, the main lobby, the auditorium and a clock tower that enhances the principal

façade. Is the other bodies, the central is practically solved with pilasters and piers, and there are few

bearing walls. It is composed by basement, ground floor, first floor, second floor and attic. The ceilings

of the basement and the ground floor are solved with spans no greater than 5 m.

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Figure 2.8 - Lobby

• West body

It has basement, sub basement, ground floor, first floor, second floor and attic. Form the basement to

the first floor, the body is divided by two longitudinal spaces. The ceilings are a succession of “quatre

punts” vaults supported by the interior bearing walls, the arches of the façade and the arches between

the two successive vaults. The ceilings of the second floor and the attic are solved with steel beams

and tiles, covering spans of more than 9.5 m.

• Extreme West Body

It has basement, a mezzanine, ground floor, first floor, second floor and attic. The ceiling of the

basements is covered by two “quatre punts” vaults, while the one of the first floor is covered by two

ribbed vaults. In both cases the vaults cover spans of 8.8 m x 8.8 m, and are separated by circled

arch. The spaces of the mezzanine and the ground floor are covered by unidirectional steel beams

with tiles. On the second floor and the attic, the ceilings are covered by segmented timbrel vaults

supported by steel beams.

• East Body

This body is symmetric to the west body. The only main differences are differences in the geometry of

some ribs of the vaults and the decorative elements. The attic also has some important differences do

to a recent intervention.

• Extreme East Body

This body, as well as the structural distribution, is symmetric with the one located on the west side.

The vault analyzed in this thesis is located on the basement of this body (Figure 2.9). It is a “quatre

point” timbrel vault, with a quadrilateral plan and very segmented, covering spans of 8,8m x 8,8m.

Unlike the vaults located on the extreme west body, the unions of the vaults with the walls are made

with pendentive arches (Figure 2.10).

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Figure 2.9 - Vault case of study

Figure 2.10 - Vault pendentive arches

2.3.2 Structural System

The structure, in general, consists of a system of brick bearing walls and timbrel vaults with different

geometry. In some areas, the ceilings are also covered with unidirectional steel beams with tile vault.

On Figure 2.11 it is shown the structural scheme of the Administrative Building basement.

The vertical loads are supported by brick bearing walls. The vault thrusts are counteracted by a

metallic structure hidden within the bearing walls, serving also, as Domenech states, to “stop vertical

movements by breaking the unbalanced loads resulting from doors and windows hollows and vertical

settlements” (Memoria, s.d. AHSCSP, 206).

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Figure 2.11 - Structural system of the basement. Timbrel vaults are shown in red while steel beams

with tile vaults are shown in blue [BOMA, 2007].

(a)

(b)

Figure 2.12 - 3D of the Administration Building structure. (a) Vaults, (b) Metallic elements [ONL].

On Figure 2.12 (a) it is shown all the vaults that cover the ceilings of the Administrative Building. On

Figure 2.12 (b) it is shown the metallic structure within the walls. The almost 115 vaults conforming the

building have their own metallic system, being simple horizontal beams surrounding the vault, vertical

elements supported on pillars, complex tie rods, etc. [Moreno et al, 2011].

Based on Domenech’s drawings (Figure 2.13) and the visual inspections made during the restoration

process of the Pavilion, the hidden metallic structure of the Extreme East Body was exposed. Above

the basement, there are two large double-height spaces, in which every space is the sum of two

square spaces separated by a large arch that, apparently, rests on two pillars and these in two

corbels, but that does not works as such because is reinforced on its interior. On Figure 2.13b it is

shown the metallic structure of the basement

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In conclusion, the Administrative pavilion is a building resolved with timbrel vaults richly decorated on

their intrados, strapped by a complex metallic structure that remains hidden within the wall thickness

or the air chambers. The absence of continuous columns in the interior and abutments or other

structure providing lateral support on the exterior, indicates that the structure bears only the horizontal

components of the vault thrust while the vertical component descends through the walls.

(a)

(b)

Figure 2.13 – (a) Static graphic analysis of one of the extreme bodies (AHSCSP

Volum_03_029_01_00), (b) Metallic structure drawings (AHSCSP Volum_03_086_01_00)

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3 TIMBREL VAULTS

3.1 Description

Timbrel vaults are masonry vaults made with ceramic pieces (tiles) and mortar. The tiles are wide and

thin, and are placed by the flat face with respect to the vault curve, usually in two or more layers

arranged so that they cover the joints of the adjacent layers. They can be built with very low thinness.

Usually, the ones built with two layers have 10 cm of thinness (including an intermediate layer of

mortar and the covers) while the ones with one layer are around 5 cm. The most common dimensions

for the pieces are 30 cm x 15 cm x 1.5 cm (Figure 3.1).

(a)

(b)

Figure 3.1- Stair Timbrel vault (a) First layer, (b) Placing the tiles

The fixing of the pieces is achieved by the adhesion of quick settler mortar (plaster in general). Mortar

is not a simply base for the tiles but a thick layer located between the pieces and around them, so the

resultant fabric construction is kind of a concrete made with a conglomerate of highly regular pieces.

At present, the first sheet is constructed with plaster while the additional sheets are fixed with Portland

cement mortar, material that increases the cohesive power between the unions. This improvement of

the technique was first implemented by Rafael Guastavino at the end of the XIX century, and it

allowed him to obtain larger spans with very low vault thinness [Tarragó, 2001].

They were classified by Guastavino as cohesive constructions, in which the adhesion between the

elements is the stabilizer mechanism. Because of this, the setting speed of mortar and the placement

of the pieces, they can be constructed without centering. Frequently, light trusses are used only for

controlling the geometry. Scaffolding is sometimes needed but only for supporting the workers. The

use of plaster for the first sheet offers no weather resistant but an immediate fixing of the pieces. This

sheet, when is completed, is used as support for the additional ones.

Due to their monolithic nature, these vaults thrust in low quantities, and can be build much lowered (30

cm of rise for 3-6 m of span). The slenderness ratio, the relationship between the radius of curvature

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and span, is found around one hundred and can also span large spaces, being the biggest vault the

one above the crossing of the cathedral of Saint John the Divine in New York, with a 33 m span.

Because they are build with ceramic and cement, they are completely incombustibles and do not allow

fire propagation.

3.2 History of timbrel vaults

The historic origins of this construction technique are not clear, and even if this technique is also

called volta a la catalana (catalan vault) it was also used in the region of Extremadura, Spain and

some Mediterranean regions [Collins, 2001]. It is possible that this construction technique was learned

from Mesopotamia or Egypt, because the constructive process is very similar to the ones developed in

those regions -the same that was later employed by Byzantines and Muslims-, where vaults are

constructed by successive layers without using centering [Huerta, 2004].

However, none of these civilizations placed the tiles by their flat face. The first know civilization using

tiles by their flat faces were Romans, and the constructive process is documented by Choisy (Figure

3.2). The tiles were used mainly as centering, aimed to reduce the use of wood and provide a rigid

support during the concrete vaults construction process, in order to prevent settlements, and not as a

structural system, so thick vaults were not constructed [Choisy, 1999].

Figure 3.2 - Use of tiles for concrete vault constructions by Romans [Choisy, 1999]

The first written documentation about the use of vaults made with flat bricks and plaster appeared in

Valencia, Spain, in the XIV century -as it is stated by Philippe Araguas [Bergós, 1965]-, in a text made

by Pedro IV on 1382 about the construction of the Royal Palace in Valencia (today already

demolished), but they were very common in the medieval Catalunya [Collins, 2001]. Around this time

and trough the centuries XV and XVI, timbrel vaults were mainly used on Gothic and Romanesque

constructions as severies supported by the ribs. The self supported timbrel vault construction

technique was introduced at the end of the XVI century, and was quickly spread through the Catalan

architecture during the XVII and XVIII century [Tarragó, 2001].

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Some authors propose that this technique came from Italy to Catalunya, and that stone vault

construction was replaced by timbrel vaults due to influence of the ones built in the Sistine Chapel and

the Farnesio Palace in Rome as a consequence of the general enthusiasm for the Renaissance

[Joaquin Bassegoda, 1936].

After the annexation of the Roussillon region or North Catalunya to France on 1659, French Militaries

engineers spread the timbrel vaults construction technique or voute a la Rousillon -name received by

French people- through the south of France after analyzing the existent constructions on Perpignan,

reaching years later the Languedoc region. This constructive systems was used particularly by the

duke of Belle Isle, who used some timbrel vaults for the construction of his castle on Bizy, France,

using for this purpose masons from Perpignan. The resultant vaults aroused the interest of an

enlightened nobleman, the earl Félix François d’Espie, who studied some buildings constructed with

timbrel vaults and even built one with this kind of construction. The most important advantages he

found on timbrel constructions were their incombustibility, reduced weight and adaptability. He

collected all his experiences and comments in a book called La Maniére de rendre toutes sortes

d’edifices incombustibles, published on 1754.

Figure 3.3 - Timbrel vault proposed by the earl d'Espie [Espie, 1754

Until the middle of the XIX century they were used for covering the naves of churches –supporting

only their own weight and loads due to maintenance-, to form brick noggin and for build stairs. They

were started to be use massively for the constructions of ceilings and floors of industrial buildings in

the beginning of the nineteenth century in Spain and France, and became almost a national symbol at

the end of the XIX century and the beginning of the XX century in Catalunya [Huerta, 2004].

At the end of the XIX century they were exported by Rafael Guastavino to America, where he built

some of the most important buildings in the east area of the United States between 1890 and 1900

(Figure 3.4). With more than 1000 timbrel vault constructions on his own -participating in cathedrals,

libraries, churches, train stations, etc-, Guastavino’s work is distributed on 41 states of United States

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16 ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS

and another nine countries [Collins, 2001]. Guastavino gave a more technical approach to

construction process of timbrel vaults, from the theory and practical aspects, development that allowed

him to cover big spans with this system.

Figure 3.4 - Advertise drawing showing the largest constructions built by the Gustavino company (Avery Library, University of Columbia)

At the beginning of the XX century, during Modernism, timbrel construction technique became a

medium of the architectonical expression for Catalan architects, who obtained a great diversity of

shapes that would had been very difficult to achieve with another building technique [Gonzalez, 2004].

Examples of timbrel constructions during this period are the works of Luis Muncunill and Cesar

Martinell (Figure 3.5). Domenech i Muntaner consider timbrel vaults as an element of Catalan identity.

(a)

(b)

Figure 3.5 - Timbrel vaults construction by (a) Lluis Muncunill and (b) Cesar Martinell

(http://media.rurismo.com/, 22.06.13)

But it will be Antonio Gaudi the one who will take the system and their structural application to

exceptional limits, trying to achieve a synthesis between structure and shape (Figure 3.6). One of his

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most important vaults was the ones constructed on the portico of the crypt of the Colonia Güell church,

the first ones to be built with hyperbolic paraboloid shape on the history of architecture

[Tarrago, 2001].

(a)

(b)

Figure 3.6 - Crypta Guell church timbrel vautls, (a) in the interior, (b) at the exterio portico.

Figure 3.7 - Dome in the Gijón University by Luis Moya

(http://ennegativo.blogspot.com.es, 22.06.13)

After decay of Modernism, during the 30’s, the massive use

of timbrel constructions diminish in Catalunya and its most

common application was for stair constructions. Even thou,

they were studied and used from architects abroad.

Once Spanish civil war finished, there was not good iron

supply or it was with very low quality, so the constructions

required the use of compression structures such as arches

and vaults in order to avoid the use of iron. Because of this,

timbrel constructions were retaken again but this time in

Madrid, by the Spanish architect Luis Moya, the last great

timbrel vault builder (Figure 3.7). One of his most

representative works is the Museo de América in Madrid,

where timbrel vaults are reinforced with cross arches. He

also published, on 1947, the first book about timbrel

constructions during the post-war period, Bóvedas

tabicadas.

On his visit to Barcelona on 1928, Le Corbusier got very interested on the timbrel conical shape roof of

the Sagrada Familia Schoo. It will be during the 50’s where his interest for timbrel vaults will increase,

being the Jaoul Houses (1952) his first construction with this technique, and the best evolution of his

designs with timbrel vaults the ones of the Sarabhai house (1955). All the direct references for timbrel

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vault construction techniques were provided by Domenech i Escorsa, a Catalan architect who

collaborated with Le Corbusier [Tarragó, 2001].

Figure 3.8 - Le Cobusier, (a) drawings: Sagrada Familia School (http://amf2010blog.blogspot.com.es/,

22.06.13), (b) plans of Sarabhai House (http://albaramirezarteaga.blogspot.com.es/, 22.06.13)

The influence of timbrel constructions will also reach South America, this time by the hand of another

Catalan architect named Antoni Bonet i Castellana, who travel to Argentina during the Spanish civil

war. For one of his projects in Uruguay, trying to find a solution for a reinforced concrete vault, Bonet

asked an Uruguayan engineer, Eladio Dieste, to make the calculations. After some discussions and

proposals for obtaining thicker vaults, the resulting solution was a reinforced brick vault. The idea

became after Bonet tried to explain Dieste the timbrel vault construction process used in Catalunya, a

technique he did not know properly [Tarrago, 2001]. The used bricks for this solution had 5 cm of

thickness, and reinforce were two steel bars of (4 mm of diameter) located on two transversal joints of

2 cm thick The most significant difference between reinforced brick and timbrel constructions is the

use of a slipform [Tomlow, 2000]. Some years later, Dieste improved this technique by reducing at

maximum the thickness (Figure 3.9).

Figure 3.9 - Eladio Dieste works (http://www.dieste.com.uy/, 21.06.13)

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Figure 3.10 - Mapungubwe Interpretation Centre (http://www.peterricharchitects.co.za, 21.06.13)

In the present, there has been a revival of timbrel

constructions, especially in countries under

development, due to the possibility of this

technique to use local material and the low cost

in labour. Examples of this are the Mapungubwe

Interpretive Centre in South Africa (Figure 3.10),

finished in 2009, and the Sustainable Urban

Dwelling Unit (SUDU) built in Ethiopia and

finished in 2011.

3.3 State of the art in timbrel vaults structural a nalysis

A bibliographical research about the structural analysis of timbrel or Catalonian vaults has been made

by Santiago Huerta in his article La mecánica de las bóvedas tabicadas en su contexto histórico: la

aportación de los Guastavino, that was published on the book Las bóvedas tabicadas de Guastavino

en América [Huerta, 2001], and the information exposed on this chapter is based on this article.

According to Huerta [Huerta, 2001], the first documents about this kind of construction are from the

XIV century, being the most important book about timbrel vault mechanic behaviour in this period, the

architectural treatise of Fray Lorenzo de San Nicolás, published in Madrid on 1639. In this work, the

author does not make any distinction between building a vault with stone, brick or timbrel, leaving the

decision of using the materials to the architect, but gives some empirical recommendations for the

calculation of the abutments for a church with one barrel vault nave, Latin cross plan and a crossing

covered by a dome, the most typical construction of that time (Figure 3.11).

Figure 3.11 – Church project from treatise of Fray Lorenzo de San Nicolás [San Nicolás, 1639]

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Besides, some recommendations for dimensioning the abutments are given, based on the vault

material, the span and the abutment type: continuous wall or wall with buttresses. A summary of these

recommendations are shown on Table 3-1. From this, it can be deduced that, during this period, it was

known that the only difference in the structural behaviour between the timbrel vaults and the brick or

stone vaults, was the less thrust due to the reduction in weight, and that buttresses were needed for

timbrel vaults but in smaller dimensions.

Table 3-1 – Recommendations of Fray Lorenzo for the dimensions of the abutments in function of the

span [Huerta, 1990]

Material Uniform wall wall wall+buttresses

Stone L/3 L/6 ≥ L/3

Brick L/4 L/7 L/3

Timbrel L/5 L/8 L/4

The first treatises of architecture did not distinguished between the structural behaviour of timbrel

vaults and brick or stone vaults, but after the XVII century they were considered to behave different.

The publication written by the earl d’Espie on 1754 was one of the most well received documents

about timbrel vaults construction. In one of the chapters of his book, there is a comparison between

timbrel vaults and conventional vaults and it is described how masonry vaults thrust, followed by an

advise that this behaviour does not apply for timbrel vaults due to their different nature, and attributes

the absence of thrust due to the monolithic nature of the resultant vault: a solid mass that does not

have cracks on it and cannot be divided on small portions.

Although the ideas of D’Espie about timbrel vaults thrusts were not correct, these were accepted by

later authors without criticism, which is the case of Laugier (1755), Rieger (1763), Blonde/Patte

(1771-1777) and Rondelet (1802). However, some other authors disapproved this conception, like

Ventura Rodriguez who criticizes the absence of thrust idea on the introduction of the Spanish

translation of d’Espie’s book made by Joaquín de Sotomayor (1776), and Manuel Fornés y Gurrea in

his treaties (1841,1846), who made emphasis on the need of counteracting timbrel vaults thrust on

masonry structures.

It will be Rafael Guastavino (1842-1908) -a Spanish master builder- the first one to formulate a

scientific theory explaining the structural behaviour of timbrel vaults. The importance of Guastavino

lies in the fact that he constructed more than 1000 timbrel vaults in North America, taking the

constructive technique from Spain -where he learnt this tradition- to the United States. Because this

kind of vaults were completely unknown in America and was looked with reticence by architects and

builders, he had to convince the construction guild about the resistance and quality of these

structures, making for this purpose some test to obtain values of breaking by compression, traction

and shear, shearing and bending, which allowed him to verify the safety of timbrel vaults by

comparison to working tensions (Figure 3.12).

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Figure 3.12 - Load test carried by Guastavino on 1901 (Avery Library,

University of Columbia)

For calculating the thinness arch

Where: = Area per unit of transversal length to the vault key.

� = Tension failure by compression.

= Load by sq m (includes self

l = vault span

= vault rise

This is the expression for calculating

load, which is an approximation

uniform). Because tension is higher on the springs,

new thickness, varying it from the key by

fixes the position of the point. These are equil

is used to be compared with the

can be masonry abutments or

Nevertheless, at the end of the XIX century, elastic

approach for analyzing masonry arches an

frequently, were regarded with suspic

the simplest cases, the calculations leads to solutions with complicated integrations, and for this,

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Load test carried by Guastavino on 1901 (Avery Library,

University of Columbia)

All his experience and ideas were collect on the

Theory and History of Cohesive Construction,

Especially to the Timbrel Arch (published on 1892),

exposes the theories that gave an historical and academic

background to his timbrel constructions. In this essay, he

divides masonry construction in two groups

mechanical behaviour: mechanic construction or by gravity and

the cohesive construction or by assimilation, framing the timbrel

constructions as cohesive ones, because of the resistant

product obtained from the good adherence between the tiles

and the mortar. Also, in this essay, he deals with

barrel vaults and semicircular domes thrusts,

of domes as half of a barrel vault thrust with the same profile.

arches and segmental vaults, the following expression is given:

��� � �

8�

= Area per unit of transversal length to the vault key.

= Tension failure by compression.

= Load by sq m (includes self-weight, filling and overload).

This is the expression for calculating the key thickness of a parabolic arch

oad, which is an approximation but serves really well for segmental vaults (the r

is higher on the springs, he applied Dejardin formulation

new thickness, varying it from the key by a function of the inverse of the cosine of the angle which

fixes the position of the point. These are equilibrium calculations that give as result a thrust value that

with the material resistance and for calculating the counteracting system, than

masonry abutments or cast iron ties.

Nevertheless, at the end of the XIX century, elastic calculations were considered to be

approach for analyzing masonry arches and equilibrium calculations, even if they were used

frequently, were regarded with suspicion by engineers of that time. With the Elastic approach, even for

culations leads to solutions with complicated integrations, and for this,

ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS 21

ce and ideas were collect on the Essay on the

Theory and History of Cohesive Construction, Applied

(published on 1892), where he

that gave an historical and academic

background to his timbrel constructions. In this essay, he

onry construction in two groups according to its

behaviour: mechanic construction or by gravity and

the cohesive construction or by assimilation, framing the timbrel

, because of the resistant

d adherence between the tiles

, he deals with segmental

thrusts, considering thrust

barrel vault thrust with the same profile.

segmental vaults, the following expression is given:

parabolic arch supporting a uniformed

the real load is not exactly

Dejardin formulation for calculating the

a function of the inverse of the cosine of the angle which

ions that give as result a thrust value that

calculating the counteracting system, than

ns were considered to be the best

equilibrium calculations, even if they were used

the Elastic approach, even for

culations leads to solutions with complicated integrations, and for this,

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22 ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND

Guastavino commissioned an applied mechanics professor from MIT, Gaetano Lanza (1891), the

elaboration of a table for the elastic calculations of timbrel vault stresses, with a rise

1/10, considering the normal force and the bending moment. The table is included at the end of his

book, without any explanation about the calculation hypothesis.

By this time, Rankine had already formulated the basic equations for the

[Rankine,1858], useful for timbrel domes, but its application to shells of any shape came with the

graphic method developed by Eddy (1878) that became

This method was the one used by Rafael Guastavino Expósito (1873

father since he was fifteen- for the calculation of timbrel dom

zones and reinforce them.

Thanks to Dunn’s observation that, in a masonry vault without reinforcements, from the point of

traction apparition the thrust will stay constan

dome without tractions in which the upper part is

directions with a modification of the dome’s

tractions appears, idea that he later patented on 1910. The result is a dome with a simple geometric

shape in the upper zone with a deviation, when it is necessary, in the base area

(a)

Figure 3.13 - Guastavino Moreno Espósito drawings

graphic analysis for the Saint John Divine Dome, (b) patent for reinforce

On the other hand, Antonio Gaudí also used equilibrium analysis for his projects, employing graphic

static methods for the simple cases and hanging m

the Sagrada Familia and the Guell Crypt

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Guastavino commissioned an applied mechanics professor from MIT, Gaetano Lanza (1891), the

elaboration of a table for the elastic calculations of timbrel vault stresses, with a rise

1/10, considering the normal force and the bending moment. The table is included at the end of his

book, without any explanation about the calculation hypothesis.

By this time, Rankine had already formulated the basic equations for the equilibrium analysis of shells

, useful for timbrel domes, but its application to shells of any shape came with the

d developed by Eddy (1878) that became popular in America by Dunn (1904,1908).

This method was the one used by Rafael Guastavino Expósito (1873-1950) -who worked with his

for the calculation of timbrel domes, basically, to determine the traction

Thanks to Dunn’s observation that, in a masonry vault without reinforcements, from the point of

traction apparition the thrust will stay constant, Guastavino Espòsito developed a design method of

dome without tractions in which the upper part is a spherical cap working by compression in all

with a modification of the dome’s plan from the shearing diagram on the point where

tractions appears, idea that he later patented on 1910. The result is a dome with a simple geometric

pper zone with a deviation, when it is necessary, in the base area (Figure

(b)

Guastavino Moreno Espósito drawings (Avery Library, University of Columbia)

for the Saint John Divine Dome, (b) patent for reinforcement of tension

domes

audí also used equilibrium analysis for his projects, employing graphic

static methods for the simple cases and hanging models for the complexes ones like

and the Guell Crypt (Figure 3.14).

vault of the Administration building of the Hospital Sant Pau

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HISTORICAL CONSTRUCTIONS

Guastavino commissioned an applied mechanics professor from MIT, Gaetano Lanza (1891), the

elaboration of a table for the elastic calculations of timbrel vault stresses, with a rise-span relation of

1/10, considering the normal force and the bending moment. The table is included at the end of his

uilibrium analysis of shells

, useful for timbrel domes, but its application to shells of any shape came with the

popular in America by Dunn (1904,1908).

who worked with his

es, basically, to determine the traction

Thanks to Dunn’s observation that, in a masonry vault without reinforcements, from the point of

a design method of a

y compression in all

n the point where

tractions appears, idea that he later patented on 1910. The result is a dome with a simple geometric

Figure 3.13).

(Avery Library, University of Columbia): (a) Static

ment of tension zones in

audí also used equilibrium analysis for his projects, employing graphic

the ones used for

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Figure 3.14 - Reproduction of Gaudí hanging model on the Museum of the Colonia Guell (Picture

taken by Adeliya Agzamova)

As it was stated before, at the end of the XIX century, Elastic analysis was considered the best

approach for masonry arches, and the ideas of continuity, tension and resistance to bending moments

fitted well with the ideas of monolithism and cohesion, so the emphasis of timbrel vaults was on the

resistance to traction and bending moments. The first one that discussed the need to consider the

bending resistance of timbrel vaults was José Domenech i Estapá (1900), who considered that timbrel

vault success, came from their capacity to resist bending which can nullify horizontal thrust.

Even thou, the first person to propose the timbrel vault analysis as elastic arches was Jaime Bayó

(1910) by assimilating them as two hinged iron arches, reducing the problem to finding what he calls

the “funicular of elasticity forces”, the lines of thrust that besides being in equilibrium with loads

complies with the conditions of elastic compatibility of deformation. For this, Bayó gives the formulas

for the usual integrals and explains a graphic procedure for the resolution of symmetric arches with

constant or variable thickness, and another one for asymmetric arches.

Also, on 1910, Cardellach, on his book about the philosophy of structures [Cardellach, 1910],

considers timbrel vaults as cohesive and highlights their capacity to resist bending, to which he

attributes the infinite variety of forms than can be built. The first person to try an elastic analysis on a

timbrel vault more complex (a stair vault on horseback) was Esteve Tarredes, engineer and

mathematician, who tried to resolve the timbrel vaults calculation problem but he failed due to the fact

that the approach to elasticity equilibrium equations for a spatial structure is very complex, even for a

simple structure. By this time, timbrel vaults were considered impossible to calculate.

Years later, Josep Goday during his speech on 1934 to the Academia Catalana de Belles Arts de Sant

Jordi, made a historical review of timbrel vault calculation, accepting Guastavino’s cohesive ideas and

Bayó and Terradas approach of considering timbrel vaults as thin elastic continuous shells within the

elasticity theory. Eduardo Torroja on his book Razón y ser de los tipos estructurales (Reason and

being of structural types), published on 1956, reproduces this opinion when talking about timbrel

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vaults, arguing that its behaviour and its resistance was very difficult to explain with actual theory

knowledge, but it was easily intuited by their constructors [Torroja, 1976]. Also Bassegoda makes

similar considerations on his numerous contributions regarding timbrel vault constructions.

On the other hand, Luis Moya (1947) recognizes the insufficiency of calculations due to a lack of data

regarding the elastic constants of timbrel vaults, so makes his equilibrium calculations using thrust

lines, methods enough for him to design and build his vaults.

Bosch (1947) defended the membrane analysis and proposed a system to calculate timbrel

pendentive vaults thrust by imaging the formation of virtual cross ribs on which, in turn, elemental

arches produced by doing parallel cuts on the arches of the contour would rest, an equilibrium method

that seeks a possible state of compression within masonry. Bergós (1936, 1953, 1965) dedicated

several years to the investigation of walls and timbrel vaults mechanical properties, performing tests

on timbrel arches to justify the application of the elastic theory, but on his books, the practical

examples are solved using thrust lines graphical methods, this is, equilibrium methods.

Angel Pereda Bacigalupi (1951) published on of the lasts books about calculation of timbrel vault

calculation, supposing, like Bayó, two-hinged arches on rigid bearing and calculates them with the

usual formulas of elastic arches, and explicitly seeks such a thickness that the line of thrusts is

contained within the central third, reducing by this the admissible tensions of traction, showing a better

knowledge of the material properties superior to previous predecessors in elastic design.

On the present, Finite Element Models are applied for timbrel vaults analysis with the consequences

of being very sensible to small variations on the boundary conditions. Non-linear analysis improves the

model but this continues being sensible to the structure load history, crack propagation on unexpected

areas, boundary condition variations, etc, so the results with this models must be well analyzed and

compared with experimental and real data.

An advance funicular 3D extension for thrust line analysis has been developed by Philipe Block

[Block, 2009] known as Thrust Network Analysis (TNA). The method finds possible funicular solutions

under gravitational loading with a defined envelop by providing a graphical solution, adopting the same

advantages as graphic statics but offering a viable extension to fully three-dimensional problems. For

this, projective geometry, duality theory and linear optimization are used. The method was inspired by

O’Dwyers’s work on funicular analysis of vaulted masonry structures.

On his article, Huerta [2001] concludes that timbrel vaults are masonry vaults with a good

compression resistance and a low traction resistance that allows them to support some bending and

the explanation of the resistance to bigger loads or for long periods of time, lies in the existence of

other resistant devices. The cohesive character is not relevant from the structural point of view, but it is

from the constructive procedure, and is the key for constructing them using only light auxiliary

elements to control the form. By this, they must be calculated within the modern Limit Analysis of

masonry formulated by Heyman, arguing that the safety problem for vaults resides on the geometrical

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shape of the structure, so the traditional proportions proposed by Fray Lorenzo, the simplified formulas

of Guastavino father, the membrane analysis of Guastavino son, the compressive elastic analysis

made by Pereda, etc, are correct, because they are no more real than any other equilibrium solution.

Figure 3.15 - Relationship between the compression equilibrium shape, the thrust network, its planar

projection and the reciprocal diagram, used for applying the TNA method [Block, 2009].

Although there has been a high interest in history to formulate a theory to calculate and predicts the

behaviour of timbrel vaults, builders were more worried about the construction process than for

calculation results, and seemed convinced that building conventional forms were safe enough, and

that the crucial problem in the designing of masonries is not resistance but geometry.

3.4 Timbrel vault typologies

3.4.1 Barrel Vault

Barrel vaults are formed by the displacement of a semicircular arch along a longitudinal axis. They are

the simplest form of vaults. They are generally used for covering elongated spaces such as churches

naves. They are known form Ancient Egypt, they were used extensively on the time of classical

Roman architecture, and continued in others cultural and artistic period such as Romanesque,

Baroque and neoclassical. They are also the most common type of vault on constructions, because of

their construction economy and their ease and speed of execution [Gulli, 2001].

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Figure 3.16 – Wall cavities for supporting the vault

The curvature is defined by the relation

between rise-span that varies from 1/12 to 1/5.

For timbrel barrel vaults constructions, it is

used a light truss that moves as the vault

construction advances, over two strips of

wood attached to the walls, or directly inserted

in them after doing some small cavities on the

walls (Figure 3.16). However, the use of this

truss is not indispensable.

For vaults covering large spans, the construction process is aided by a guide made of strings fixed to

two centerings that are placed at the vault ends, and is used basically to obtain a proper execution of

the vault curvature (Figure 3.17).

Figure 3.17 - Use of strings and light trusses for the construction of a barrel vault [Moya, 1947].

For the construction of the first layer, the tiles are bonded by arches in the directrices direction,

although, in some cases, depending on the bonding type, another procedure is adopted. For the

normal bonding, the arches are formed by placing the tiles by their maximum length and on the

generatrices direction (Figure 3.18, type A and C), sometimes they are formed by the directrices

directions (Figure 3.18, type B and D).

The first bonding adjust better to the vault shape but has the inconvenient that, when the pieces are

placed without using light trusses, it takes more time for them to stay steady due to the moment acting

over the piece, resulting from the higher distance to the pivot. If a light truss is used, this problem

disappears.

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Figure 3.18 – Bondig types following: A and C, Generatrices direction; B and D, Directrices Direction

Usually, the group of workmen builds the first layer stopping at the proximity of the free edge of the

vault, progressing no more than 60 cm (an extent easily reached by the hand of a worker) so the

scaffolding can be used for constructing the following l

layers starting on the imposts till the vau

the previous layers [Gulli, 2001].

Figure 3.19 - Ribs on barrel vaults surface

[Moya, 1947].

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Bondig types following: A and C, Generatrices direction; B and D, Directrices Direction

[Truñó, 2004].

Usually, the group of workmen builds the first layer stopping at the proximity of the free edge of the

vault, progressing no more than 60 cm (an extent easily reached by the hand of a worker) so the

scaffolding can be used for constructing the following layers. It is important to extend the consecutive

layers starting on the imposts till the vault key is reached, and place the pieces breaking the joints of

[Gulli, 2001]..

Ribs on barrel vaults surface

Figure 3.20 - Possible deformation by buckling

[Choisy, 1999]

ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS 27

Bondig types following: A and C, Generatrices direction; B and D, Directrices Direction

Usually, the group of workmen builds the first layer stopping at the proximity of the free edge of the

vault, progressing no more than 60 cm (an extent easily reached by the hand of a worker) so the

ayers. It is important to extend the consecutive

, and place the pieces breaking the joints of

Possible deformation by buckling

[Choisy, 1999]

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28 ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS

If the curvature of the vault is too lowered, it is necessary to construct ribs in the direction of the

generatrices of the vault for counteracting the traction forces and stiffen the structure on the horizontal

direction (Figure 3.19). The spandrel of the vault must be filled in order to avoid the risk of buckling

deformations by tangential loads. Usually, they are filled with earth and ceramic elements, but

lightweight concrete can also be employed (Figure 3.20).

3.4.2 Cross vault

Cross vaults are the ones resulting from the intersection of two barrel vaults at right angles.

Geometrically, they are generated by two orthogonal semicylindrical surfaces whose intersection lines,

or arrises, are ellipse arches crossing on the upper vertex. The vault shape allows an easy distribution

of the thrusts generated by the roofs to the walls. It was first exploited by Romans and became one of

the most important covering system during Romanesque period. Abandoned on Gothic period by rib

vaults, they were recuperated during Renaissance. Together with the barrel vault, is one of the most

common types of vault [Gulli, 2001].

(a)

(b)

Figure 3.21 - Timbrel cross vault building processes [Moya, 1947].

There are two methods for building cross vaults. The simplest one is done by positioning light trusses

on the diagonals direction –being supported on the four lateral walls-, indicating the starting of the

vault in accordance to the four correspondent arches and constructing every portion of the vault by

disposing auxiliary strings –serving as generatrices- between two of the arches and their

corresponding truss (Figure 3.21 a).

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The second method consist on

so an horizontal plane, in which

the arches are drawn over the lateral walls and the trusses are placed along the diagonals. Then, the

vault generatrices can be defined using hanging plumbs in every horizontal string, pointing for every

generatrix, a fixed distance betw

For understanding the construction process

Construcción de bóvedas tabicadas

constructed (A C B D) starting,

the tiles 1 and 2, and continuing placing complete pieces until

will be supported by the walls and the diagonal trusses. After this, the second l

placed, forming a second arch (2, on

layer can be started (3, on Figure

first layer), can be started, placing after finishing it the second layer (5, on

layer (6, on Figure 3.23 a). The constructions of additional arches must not be performed till the

previous ones are finished.

Figure 3.

uctural Analysis of a vault of the Administration building of the Hospital Sant Pau

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The second method consist on raising the four edge walls, surpassing the key elevation of every arch,

which can be fixed a system of tensed strings- can be obt

over the lateral walls and the trusses are placed along the diagonals. Then, the

vault generatrices can be defined using hanging plumbs in every horizontal string, pointing for every

generatrix, a fixed distance between them and the horizontal plane (Figure 3.21

understanding the construction process it will be used Figure 3.22, taken from Angel Truñó’s book

Construcción de bóvedas tabicadas [2004] .Once the trusses are placed, the first set of arches can be

constructed (A C B D) starting, simultaneously, at the starting points F E H G,

and continuing placing complete pieces until finishing the four arches

supported by the walls and the diagonal trusses. After this, the second l

placed, forming a second arch (2, on Figure 3.23 a). Once the second arches are formed, the third

Figure 3.23 a). By this, the second set of aches A´4, (second arch of the

first layer), can be started, placing after finishing it the second layer (5, on Figure

). The constructions of additional arches must not be performed till the

.22 - Cross vault construction process [Truñó, 2004].

ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS 29

surpassing the key elevation of every arch,

can be obtained. After this,

over the lateral walls and the trusses are placed along the diagonals. Then, the

vault generatrices can be defined using hanging plumbs in every horizontal string, pointing for every

21 b).

from Angel Truñó’s book

Once the trusses are placed, the first set of arches can be

simultaneously, at the starting points F E H G, by cutting and placing

the four arches. These arches

supported by the walls and the diagonal trusses. After this, the second layer is immediately

). Once the second arches are formed, the third

). By this, the second set of aches A´4, (second arch of the

Figure 3.23 a) and the third

). The constructions of additional arches must not be performed till the

[Truñó, 2004].

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30 ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND

(a)

Figure 3.23 - Constructive process: (a) layers setting, (b) Arrise formation [Truñó, 2004].

On the arrises, the tiles of the first layer are cut in a shape similar to the intersection. For the additional

layers, a scaling is formed in order to obtain a discontinuity on the joints. Finally, on the extrados, a

source of brick is placed at both sides of the intersection

3.4.3 Cloister vaults

Cloister vaults results from the intersection of two barrel vaults crossing in right angle with the

circular shapes, so there are obtained elliptical arches on the corner. It is named because it was built

only, on its beginning, in cloisters or in crossing corridors with barrel shape. It is a very common vault

on the Spanish Romanesque.

For explaining the construction process,

installing the trusses on the diagonals

needed, they can be braced with elements in the generatrix direction, so the geometry of the shape

can be better defined (FG GH). There can be also used trusses with the

supporting vault portions (IJ JK). The

the generatrices of each vault. The most common bonding types are also shown on

The portions of the vault are constructed by arches that have their counteracting on the arches of the

consecutive portion vault. By this, the shape is supported by itself, and can be built without using

additional supporting elements. The construction of the arches beg

it is indicated on the arches TT UU VV etc. The placing order of the tiles for the bonding AIJK and

BLMN must be followed till the vault is completed.

Structural Analysis of a vault of the Administration building of the

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(b)

Constructive process: (a) layers setting, (b) Arrise formation [Truñó, 2004].

On the arrises, the tiles of the first layer are cut in a shape similar to the intersection. For the additional

scaling is formed in order to obtain a discontinuity on the joints. Finally, on the extrados, a

source of brick is placed at both sides of the intersection (Figure 3.23 b).

from the intersection of two barrel vaults crossing in right angle with the

, so there are obtained elliptical arches on the corner. It is named because it was built

on its beginning, in cloisters or in crossing corridors with barrel shape. It is a very common vault

For explaining the construction process, Figure 3.24 will be used. The first procedure

the trusses on the diagonals -with the elliptical shape- on the corners (CB CD CE CA). If it is

, they can be braced with elements in the generatrix direction, so the geometry of the shape

can be better defined (FG GH). There can be also used trusses with the directrices shape of the

vault portions (IJ JK). The references for placing the tiles are obtained by placing strings on

the generatrices of each vault. The most common bonding types are also shown on Figure

f the vault are constructed by arches that have their counteracting on the arches of the

consecutive portion vault. By this, the shape is supported by itself, and can be built without using

additional supporting elements. The construction of the arches begins at the ends of the diagonals, as

it is indicated on the arches TT UU VV etc. The placing order of the tiles for the bonding AIJK and

BLMN must be followed till the vault is completed.

vault of the Administration building of the Hospital Sant Pau

Erasmus Mundus Programme

HISTORICAL CONSTRUCTIONS

Constructive process: (a) layers setting, (b) Arrise formation [Truñó, 2004].

On the arrises, the tiles of the first layer are cut in a shape similar to the intersection. For the additional

scaling is formed in order to obtain a discontinuity on the joints. Finally, on the extrados, a

from the intersection of two barrel vaults crossing in right angle with the same

, so there are obtained elliptical arches on the corner. It is named because it was built

on its beginning, in cloisters or in crossing corridors with barrel shape. It is a very common vault

will be used. The first procedure consists on

(CB CD CE CA). If it is

, they can be braced with elements in the generatrix direction, so the geometry of the shape

directrices shape of the for

he tiles are obtained by placing strings on

Figure 3.24.

f the vault are constructed by arches that have their counteracting on the arches of the

consecutive portion vault. By this, the shape is supported by itself, and can be built without using

ins at the ends of the diagonals, as

it is indicated on the arches TT UU VV etc. The placing order of the tiles for the bonding AIJK and

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Figure 3.24 - Ti

3.4.4 “Quatre punts” vault

These vaults are obtained by the rotation of a curve generatrix, always contained on a vertical plane,

over curve directrices. The generatrix and directrix curves can be

curvature. The name is given due to

step is to make perforations on the walls with the curvature of the directrices arches for supporting the

tiles. If the generatrix arch has constant curvature, it can be used a truss, working in the same was as

with the barrel vaults. If it is of variable curvature, some trusses must be used to adjust better the vault

shape.

For having double curvature, the bondi

parallel arches on the lower dimension, or by parallel arches on the higher dimension (

One of the most rational bonding types is the one shown on

braking the joints it can be done withou

For the bonding types on Figure

uctural Analysis of a vault of the Administration building of the Hospital Sant Pau

ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS

Timbrel Cloister vault construction process [Truñó, 2004].

“Quatre punts” vault

These vaults are obtained by the rotation of a curve generatrix, always contained on a vertical plane,

over curve directrices. The generatrix and directrix curves can be circled or elliptical, or with variable

curvature. The name is given due to the four rises that this vault has. For their construction, the first

step is to make perforations on the walls with the curvature of the directrices arches for supporting the

s. If the generatrix arch has constant curvature, it can be used a truss, working in the same was as

with the barrel vaults. If it is of variable curvature, some trusses must be used to adjust better the vault

For having double curvature, the bonding of the pieces can be done in both directions, by forming non

parallel arches on the lower dimension, or by parallel arches on the higher dimension (

One of the most rational bonding types is the one shown on Figure 3.25 b

it can be done without using trusses, but is advisable their use to refine the shape.

Figure 3.25 a, the construction process is the same as for

ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS 31

mbrel Cloister vault construction process [Truñó, 2004].

These vaults are obtained by the rotation of a curve generatrix, always contained on a vertical plane,

circled or elliptical, or with variable

the four rises that this vault has. For their construction, the first

step is to make perforations on the walls with the curvature of the directrices arches for supporting the

s. If the generatrix arch has constant curvature, it can be used a truss, working in the same was as

with the barrel vaults. If it is of variable curvature, some trusses must be used to adjust better the vault

ng of the pieces can be done in both directions, by forming non

parallel arches on the lower dimension, or by parallel arches on the higher dimension (Figure 3.25).

b, placing the pieces by

heir use to refine the shape..

, the construction process is the same as for barrel vaults

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32 ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND

Figure 3.25 - Timbrel "quatre punts" vault construction

3.4.5 Stairs vault

The most common use of timbrel vaults is stair construction

are constructed -being each of them

reached. The directrices are curves draw

tacit rules which are the followings:

1) Overload must be limited, so a low rise must be given to the vault.

2) Support, if possible, a symmetric load distribution.

3) The vault must serve not only

superior vault.

The first step prior the construction is drawing

that enclosure them (Figure 3.27).

veneer, by placing it tangent to the parallel EF and

minimum distance from the veneer to the inferior slope

satisfactory curvature is obtained, moment in which

inferior face of the wood veneer, that is retired when the drawing process is finished

From points B and D, the lines AB and DC are draw, following the

footprint.

Structural Analysis of a vault of the Administration building of the

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ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS

Timbrel "quatre punts" vault construction process [Truñó, 2004].

The most common use of timbrel vaults is stair construction (Figure 3.26). For this, ind

being each of them supported by the previous one- until the required elevation is

reached. The directrices are curves drawn by “feeling” or by experience, and are subjected to certain

Overload must be limited, so a low rise must be given to the vault.

sible, a symmetric load distribution.

not only as support for steps and landings, but as support for the

or the construction is drawing steps and landings on the wall and two parallel lines

After this, the vault curvature is drawn on the wall

veneer, by placing it tangent to the parallel EF and folding the ends so it pass by points B and D. The

minimum distance from the veneer to the inferior slope has to be checked. The process continues

, moment in which is marked by a thin layer of plaster placed on the

, that is retired when the drawing process is finished

From points B and D, the lines AB and DC are draw, following the slope of the vault thick and the step

vault of the Administration building of the Hospital Sant Pau

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s [Truñó, 2004].

For this, independent vaults

until the required elevation is

subjected to certain

as support for steps and landings, but as support for the

and two parallel lines

n on the wall using a wood

g the ends so it pass by points B and D. The

. The process continues till a

n layer of plaster placed on the

, that is retired when the drawing process is finished(Figure 3.28).

slope of the vault thick and the step

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Figure 3.26

Figure 3.27

The construction is made by forming arches

The first layer is made with plaster and the followings with cement mortar. The first vault of a

supported by a massive body (O) with

uctural Analysis of a vault of the Administration building of the Hospital Sant Pau

ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS

– Timbrel stairs vault longitudinal section [Truñó, 2004].

27 - Timbrel stair vault directrix drawing [Truñó, 2004].

construction is made by forming arches following the directrix BGD, and without using centerings

The first layer is made with plaster and the followings with cement mortar. The first vault of a

supported by a massive body (O) with a corresponding foundation (P). On the other end, the vault is

ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND HISTORICAL CONSTRUCTIONS 33

[Truñó, 2004].

[Truñó, 2004].

, and without using centerings.

The first layer is made with plaster and the followings with cement mortar. The first vault of a stair is

. On the other end, the vault is

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supported on incisions that are previously carved on the wall (CD). For supporting a new vault on the

inferior one, the first pieces of every layer of the new one are placed directly on the layers of the

existing one (Figure 3.29). If a vault more precise is required or faster work is needed, light trusses

can also be used.

Figure 3.28 - Use of the wood veneer for drawing the generatrix

Figure 3.29 – Support of a timbrel stair vault over an existing one.

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4 STRUCTURAL ANALYSIS OF HISTORICAL CONSTRUCTIONS: ADVANCED

APPROACHES

4.1 History and challenges

The first person to discover the ideal shape of a masonry arch in equilibrium was Robert Hooke, who

stated that it was the inverted shape of a hanging flexible line: the catenary. On 1698, David Gregory

extended Hooke´s assertion saying that arches are stable if a catenary can be fitted within their

thickness. This analogy, of analysing the equilibrium of masonry arches with the funicular models was

used during the XVIII, XIX and the beginning XX century, for the design of masonry bridges and

buildings.

During the XVII century, Coulomb publishes the first general theory on the stability of arches, providing

a mathematical approach for the different collapsing modes and proposing a way to determine the

most unfavourable sections of rupture [Coulomb, 1773]. On the other hand, Couplet established that

the collapse of an arch occurs when there are formed enough hinges as to become a mechanism

[Heyman, 1976].

On XIX century the introduction of the thrust line theory and graphics statics developed further the

methods for analyzing masonry structures, and it was used till the beginning of the XX century, when it

was displaced by the elastic theory.

All this historical insights will be synthesized by Heyman on his Limit Analysis theory. According to

this, the behaviour of masonry structures can be analysed by the following hypothesis [Heyman,1999]:

1) Masonry has no tensile strength.

2) Masonry has infinite compression strength.

3) Sliding between parts is impossible.

These conditions enables the enabling the formulation of the lower bound theorem: the structure is

safe if a statically admissible state of equilibrium can be found, in other words, it will not collapse if a

thrust line can be found within the boundaries of the structure. Even if this method describes in a

realistic way the safety and collapse of structures, it can only be used to assess the stability and safety

of structures.

According to Roca et al. [2010], the use of advanced approaches for the analysis of historical

constructions was initiated by the study of the Brunelleschi Dome by Chiarugi et al [1993]., the Pisa

Tower by Macchi et al. [1993], the Colosseo in Rome by Crocci [1995], Mexico Cathedral by Meli and

Sánchez-Ramírez [1995] and San Marco’s Basilica in Venice by Mola and Vitaliani [1995], By that

moment, the use of computer methods for the analysis of steel and concrete structures, even for

non-linear studies, was in an advanced stage, while for the analysis of historical constructions, it was a

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difficult task. The main difficulties were to describe the properties of materials, structural arrangements

and preservation condition. Today, analyzing ancient constructions is still a challenging study, and

investigations on historical structures must be integrated with complementary activities, involving

detailed historical researches in order to obtain different approaches and sources of evidence

[Roca et al, 2010].

Figure 4.1 – Mexico City Cathedral FEM [Meli and Sánchez-Ramírez, 1995]

The main difficulties are associated with the following aspects [Roca et al, 2010]:

• Material: materials used for ancient constructions such as earth, brick, stone and wood are

very heterogeneous, and is difficult to characterize and describe, mathematically, their

mechanic and strength (except in the case of wood). Brick, for example, is highly sensitive to

the orientation of the loads. The problem of characterization has been solve, in par,t by the

use of Non-destructive tests (NDT) and minor destructive tests (MDT), but only limited and

partial data can be collected, and assumptions regarding the morphology and the material

properties must be done for the model elaboration.

• Geometry: elements of historical construction usually have complex geometry, which is the

case of arches, vaults, pendentives, fillings, etc. However, this is the least challenges of the

computer based analysis, because geometry can be easy accurately modelled.

• Morphology: this problem is associated with the internal morphology of structural elements

and their internal connections and compositions, such as metal connectors, fillings, cavities,

material layers, etc. Modelling these elements is a difficult process, very demanding from a

computational point of view; even to physically characterize them by tests is not easy.

• Actions: historical constructions experiences different kind of actions since the first moment

they were erected and through all their life, such as long term gravity forces, earthquakes,

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environmental effects, anthropogenic actions, etc. Usually, these effects have a high level of

uncertainty and need to be characterized in historical time.

• Damage and alterations: existing damages and general alterations can influence the

response of the structure, and they must be modelled to predict a more realistic behaviour and

have a good construction performance.

• History: some aspects related with the history of the building need also to be taken into

account such as natural disasters, long term decay, construction process, architectural

alterations and additions, etc. The study of these actions, can lead to a better understanding

of the building performance and strength. Knowing the behaviour of the constructions in the

past, makes up for the mentioned data insufficiency.

4.2 Types of modelling

4.2.1 Elastic Linear Analysis

This method is most commonly used for calculations of steel and reinforced concrete structures, and

its application to masonry structures is not recommended because it does not take into account non-

tension response and other properties of masonry behaviour. This procedure is very conservative and

is not useful, for example, for estimating the ultimate response of masonry structures, so it not should

be used to conclude about the strength or structural safety of a structure. However, its use has been

as an auxiliary tool on the diagnosis of large structures, due to the reduced computer cost

[Roca et al., 2010].

Figure 4.2 - Linear elastic analysis of the Güell Colony Crypt [Roca, 1998

Non-linear analysis is becoming more popular thanks to the increasing in computer capacity and

software availability, but linear analysis is usually performed first in order to have an initial evaluation

of the model characterization.

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4.2.2 FEM based approaches. Macro-Modelling

Finite Element Models offers a variety of possibilities for describing masonry structures, especially for

non-linear analysis. Macro-modelling is the most popular approach because it does not need high

calculations demands as other methods (e.g. micro-modelling). It is better use for large structural

members, full constructions where a detailed description of the interaction between the brick units and

mortar is not needed. In this case, the material is characterized as a fictitious homogeneous

orthotropic continuum. This type of modelling offers significant advantages, as the FE meshes are

simpler, and is the most valuable when a compromise between accuracy and efficiency is needed.

Even thou, they have a significant limitation when modelling strong discontinuities between parts of

the constructions is needed (physical joints or individual cracks).

4.2.3 FEM based approaches. Discontinuous Models

This approach is a response of the FEM macro-modelling limitations. In order to correct them, there

are included, within the FEM mesh, joint-interface elements that models the response of

discontinuities. One of the first applications was made by Mark et al. on the study of the Hagia Sophia

buttresses (Istanbul), by combining large blocks with interface elements to allow the sliding along the

large blocks shaping the structure.

Figure 4.3 - Discontinuos model [Pegon, et. al, 2001]

4.2.4 FEM based approaches. Micro-Modelling

In this approach, the different components, units and mortar, and the unit/mortar interface are

distinctly described. The units and mortar are modelled by continuum finite elements, while the

interface by discontinuous elements represented by potential crack or slip plane. Is the most accurate

tool available to simulate the real behaviour of masonry structures, and is particularly adequate for

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describing local responses. The results obtained with this approach are very accurate due to the

detailed description of the model, but it also demands high computational resources, so its applicability

is mainly for small elements or small structure details.

Figure 4.4 - Modelling strategies [Lourenço, 1996].

4.3 Shell structures

4.3.1 Introduction to shell structures Elastic Theo ries development

Before the introduction of structural mechanics, architects and builders in general used proportion

rules to design their structures. But during the late XIX century, after the theoretical knowledge and

experience gained, a new approach for calculating shell structures, based on the elastic theory

appeared. On 1888, August Edward Hough Love derived the first basic shell equation describing the

behaviour of thin elastic shell structures based on the Kirchhoffean thin plate assumptions. It was

basically, an extension of the plate theory to structures with surface-like geometries. In 1912,

H. Reisner found that the bending and the membrane solutions can be obtained separately, and the

total solution could be obtained by the superposition of both.

During this time, there were use only simple geometrical shapes because irregular ones where almost

impossible to calculate by hand. On 1950, Heinz Isler, a Swiss engineer, derived the shell shape from

experiments with physical models like hanging fabric or inflatable rubber membranes, experiments

based on the hanging models of the early shell builders. At the same time, researches at the Frei

Otto’s Institute of Lightweight Construction at Stuttgart University, experimented with form-finding

methods for tensile systems using soap bubbles and other methods.

Until the present day, the theory of shells and physical models of Isler and Otto are extended by

computational design and analysis methods.

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4.3.2 Advanced approaches: shell historical constru ctions

According to Milani et. al [2008], when dealing with the study of complex 2D curved masonry shells,

FE approaches in the inelastic range are preferred. The most common assumptions for masonry are:

no tension resistance [Luchessi et al.199, 1997], damaging [Creazza et al, 2000, 2002]. or an

orthotropic elasto-plastic behaviour with low tensile resistance [Lourenço 1997, 2005]. In the case of

vaulted structures, few non-linear developments have been produced, because of the difficulties that

carry modelling curved structures with two dimensional and spatial characters. Among the first works

of this kind of structures, was the model of the San Marco Basilica domes by Oñate et. al.[1995],

where the vaults were modelled by means of a continuum damage model for masonry and concrete

under mechanical and other deterioration effects. In the case of analysis of the Cathedral of Santa

Maria, in Vitoria, Spain, by Croci et al.[1998], the main transverse sections of the building and the

nave vaults were analysed by and followed an incremental strategy to account for cracking due to

tension or shear stresses, as well as the equilibrium second order effects.

Figure 4.5 - Study of Saint Marco’s domes in Venice [Oñare et al., 1995].

Some FE models were used to analyse Gothic cross vaults by Barthel [1993], and they were

combined with partial constitutive models enabling the simulation of masonry cracking as well as

sliding between arch ring joints. Also Cauvin and Stagnitto [1993, 1995] carried studies on the central

nave of Reims Cathedral, by using limit analysis and FEM non-linear analysis.

A formulation based on micro-modelling technique for the study of masonry spatial and curved shells

was proposed by Lourenço [1997], where constitutive equations and stemming from plasticity to

simulate the response of the material in combination with joints elements to describe the sliding of

blocks.

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4.3.3 Advanced approaches: timbrel constructions mo delling

One of the first pioneers involving advanced approaches on timbrel vaults was Ricardo Gulli, by doing

tests on laboratory timbrel barrel vaults and comparing the results with the ones provided by Elastic

Analysis FE models, and claims that FEM is the best way of analysing this kind of structures [Lopez et

al. 2012].

Robertson performed a seismic FE analysis on the University of Berkely building constructed by

Guastavino [Robertson, 1999].

Roca, recommends the use of limit analysis and FEM macro modelling considering the nonlinearity of

the material, limited compressive strength, possible use of tensile strength (non-zero) and geometric

nonlinearity. Also, empathises on use of a precise macro modelling of the geometry.

Atamturktur et al. studied the thrust of timbrel vaults by comparing results obtained with FEM analysis

and limit analysis in two Guastavino’s constructions, using for the FE model thin-shell elements. They

advise that FEM are sensitive, so the input values must be analyzed with care

[Atamturktur et al, 2007].

Figure 4.6 - Timbrel dome FEM [Atamturktur, 2006]

Erdogmus realized non-destructive tests in a half-scale model, constructing a dome which underwent

to modal analysis and was later modelled by FE in order to understand better its behaviour

[Erdogmus, 2008]. A comparison between modelling the timbrel dome using shell elements and solid

elements was done. The results were compared with the non-destructive test data, and it was

conclude that solid elements represent the dome in a more realistic way than shell elements.

As it was mentioned on Chapter 3, the research group of John Ochsendorf with Philippe Block

developed the Thrust Network Analysis [Block, 2009], equilibrium analysis method in three

dimensions, which allows designing forms that work well using the minimum compressive material,

and can also be used for analyzing every kind of vault constructions. In the present, this seems to be

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the best approach for understanding the behaviour of timbrel constructions, because it provides a

3D analysis based on Heyman’s assumptions –being the 2D simplification one of the most criticized

aspects of the limit analysis- and is not too sensitive to boundary conditions variations –the most

discussed inconvenient of FE Analyses-.

(a)

(b)

Figure 4.7 - Timbrel dome FEM with (a) shell elements, (b) solid elements [Erdogmus, 2008].

Megan L. Reese on her Master thesis performed an structural analysis on some Guastavino’s

constructions. By comparing the results obtained from Limit Analysis, Membrane Analysis and FE

Analysis, concludes that graphical analysis are the best-suited for assessments of timbrel shells, but

recommends the use of TNA developed by Block [Reese ,2008].

Figure 4.8 - Timbrel dome FEM [Reese , 2008]

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5 FINITE ELEMENT MODEL

5.1 Software

The FE program used for the study of the vault is DIANA, a software package for finite element

analysis of structures and fluids, developed by TNO in Delft, Netherlands.

5.2 Geometry

For defining the geometry of the vault, it was used a CAD file containing a scheme of lines and

surfaces on 3D made by the company TOYSER S.A. on 2007 (Figure 5.1a). With this information, a

quart of the vault was modelled using the Rhinoceros software; the surface was generated as meshes

so when is imported to DIANA, the software interprets the resulting divisions as surfaces (Figure 5.1b).

The walls and the additional elements were generated directly on DIANA.

(a)

(b)

Figure 5.1 - Vault geometry: (a) scheme of lines by TOYSER S.A. (b) generated on Rhinoceros

5.3 Mesh Generation

For the vault modelled with the walls as boundary conditions restraining the vertical displacement, the

mesh employed is shown on Figure 5.2a. It was generated following the expected load transmission

over the vault surface, having small elements with a dense distribution near the support -where the

curvature is more pronounced-, increasing in size as they get far from the support, being the bigger

ones located on the middle and the edges of the vault.

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For the vault modelled with the bearing walls, the mesh used was the most regular possible and with

the same density in the entire structure, except on the zone between the vault curvature and the walls

linearity, where the distribution had to modified for having a better union compatibility. The mesh is

shown on Figure 5.2b.

(a)

(b)

Figure 5.2 - Model Meshes: (a) vault (b) vault and walls

5.4 Element Types

Theoretically, the most optimal FE description of a shell structure is done with the use of volume

elements. However, they are not practical for modelling shells as they have a tendency to generate

very large system of equations (producing long computational time) and they can lead to numerical

ill-conditioning problems [Zienkiewicz, 2000]. As thin 3D shell structures can be reduced to a two-

dimensional surface problem, the vault can be modelled using shell elements.

The two-dimensional surface elements offered by DIANA are based on isoparametric

degenerated/solid approach, which means that stress components normal to the vault surface are

equal to zero (plain stress assumption) and that a normal remains straight after deformation, but not

necessarily normal. The transverse shear deformation is included according to the Midlin-Reissner

hypothesis.

The surface elements chosen are QU8-CQ40S (Figure 5.3), which are 8 noded quadrilateral shaped

elements (QU8) belonging to a curved quadrilateral with 40 degrees of freedom (CQ40); the S stands

for shell elements. In this case, all the 8 nodes have 5 DOF: 3 translational and 2 rotational (the out-of-

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plane rotation is not included, so there are 5x8 DOF on the element (Figure 5.4). The elements are

based on quadratic interpolation and area integration.

The selection of this element type was done based on the fact that 8 nodes represent better the

behaviour of the vault due to its geometrical complexity.

Figure 5.3 - Quadrilateral curved shell element [Diana User's Manual, 2005].

Figure 5.4 - QU8-CQ40S curved shell elements and thier DOF [Diana User's Manual, 2005].

The steel elements were modelled as BE2-L13BE (Figure 5.5), which are 3D linear elements –based

on the Bernoulli theory- with two nodes and 13 DOF (includes an additional variable representing the

relative elongation of the beam). The transverse displacement is a cubic Hermite shape function

expressed in the nodal displacements and rotations. It is assumed that the cross-sections remain

plane and perpendicular to the slope of the beam axis. The elements are based on quadratic

interpolation and area integration (Figure 5.6).The selection of this type of element was done in order

to obtain better compatibilities with the shell elements used for the vault.

Figure 5.5 - Beam element [Diana User's Manual, 2005].

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46 ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND

Figure 5.6 - BE2-L13B beam elements and its DOF [Diana User's Manual,

For the model with the vault supported by the walls, the upper part of the walls

modelled as TR6-CT30S (Figure

element belonging to a curved triangular with 30 DOF.

area integration. In this case, the type of element was chosen for having better compatibilities with the

vault shell elements.

Figure 5.7 – Triangular curved shell element [Diana User's Manual,

5.5 Integration Schemes

(a)

Figure 5.8 - Integration scheme for (a) quadrilateral shell elements, (b) triangular shell elements

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L13B beam elements and its DOF [Diana User's Manual,

the vault supported by the walls, the upper part of the walls and the ribs,

Figure 5.7), which are six-node triangular isoparametric curved shell

element belonging to a curved triangular with 30 DOF. They are based on quadratic interpolation and

the type of element was chosen for having better compatibilities with the

Triangular curved shell element [Diana User's Manual, 2005

(b)

Integration scheme for (a) quadrilateral shell elements, (b) triangular shell elements

[Diana User's Manual, 2005].

vault of the Administration building of the Hospital Sant Pau

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L13B beam elements and its DOF [Diana User's Manual, 2005].

and the ribs, were

node triangular isoparametric curved shell

They are based on quadratic interpolation and

the type of element was chosen for having better compatibilities with the

2005].

Integration scheme for (a) quadrilateral shell elements, (b) triangular shell elements

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Over the face of the shell elements a 2x2 Gauss integration scheme is used (Figure 5.8 a), while in

the direction of the thickness an 11 points Simpson scheme is utilized. For the triangular shell

elements, the in-plane integration is made by 3 points while the thickness is integrated with 11

Simpson points (Figure 5.8 b). The high number of integration points was done to obtain a smoother

failure on the thickness, and not a brittle on, that occurs when less integration points are used. In the

case of the beam elements are used 2 points.

5.6 Material Modelling

5.6.1 Tensile Craking

On quasi-brittle materials, like tiles, the tensile behaviour is characterized by a linear elastic branch up

to crack initiation, followed by a non/linear post-cracking. This crack process is modelled with a

smeared cracking approach, where cracks appear on arbitrary locations with arbitrary orientation,

describing cracking within the elements. For each element in the mesh, when the maximum tensile

stress is reached, a crack will appear. The Rankine failure criteria was adopted (Figure 5.9).

Figure 5.9 – Rankine failure criteria in a two-dimensional stress state. [Diana User's Manual, 2005].

At the same time, the crack propagation adopted for the tile is characterized by tension in softening,

which means that the material eases up to open a crack after initiation (Figure 5.10).

Figure 5.10 - Tension in softening model [Diana User's Manual, 2005].

5.6.2 Compressive Behaviour

The compressive behaviour is modelled with a plasticity model, allowing a combination of a crack

model in tension with a yield model and a plasticity formulation in the compressive regime, so the

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48 ADVANCED MASTERS IN STRUCTURAL ANALYSIS OF MONUMENTS AND

compressive behaviour is decomposed in an elastic and irreversible plastic part.

chosen for specifying the state of stress at which the plastic flow is initiat

condition, which is especially applicable

difference in compression and tension. This is a less conservative method than the Mohr

approximation, another model for quasi

Figure 5.11 - Mohr-Coulomb and Drucker

5.7 Iterative Procedure

The Secant Method was chosen for the iterative procedure. It is a method that uses

previous solution vectors and out-of

stiffness of the structure is determined from the known positions at the equilibrium path. Because this

system has more than one degree of freedom, the secant stiffness is not unique and the stiffness

matrix must be computed with another method

Crisfield method is used.

Figure 5.12 - Secant iteration [Diana User's Manual

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compressive behaviour is decomposed in an elastic and irreversible plastic part.

chosen for specifying the state of stress at which the plastic flow is initiated was the Drucker

condition, which is especially applicable for quasi-brittle materials such as tiles, where there is a big

difference in compression and tension. This is a less conservative method than the Mohr

approximation, another model for quasi-brittle materials (Figure 5.11).

Coulomb and Drucker-Prager yield condition [Diana User's Manual

was chosen for the iterative procedure. It is a method that uses

of-balance force vectors during the increment (Figure

stiffness of the structure is determined from the known positions at the equilibrium path. Because this

system has more than one degree of freedom, the secant stiffness is not unique and the stiffness

with another method. To avoid increasing storage and computation time, a

Secant iteration [Diana User's Manual, 2005].

vault of the Administration building of the Hospital Sant Pau

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compressive behaviour is decomposed in an elastic and irreversible plastic part. The yield model

ed was the Drucker-Prager

brittle materials such as tiles, where there is a big

difference in compression and tension. This is a less conservative method than the Mohr-Coulomb

Prager yield condition [Diana User's Manual, 2005].

was chosen for the iterative procedure. It is a method that uses the information of

Figure 5.12). The

stiffness of the structure is determined from the known positions at the equilibrium path. Because this

system has more than one degree of freedom, the secant stiffness is not unique and the stiffness

. To avoid increasing storage and computation time, a

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6 MODEL DEVELOPMENT PROCESS

The model development process started by analyzing the simplest idealization of the vault, being

improved as the results obtained where not satisfactory till a model representing the behaviour of the

real structure was obtained. All the models where evaluated on the non-linear range.

6.1 Vault Description

6.1.1 Geometry

As it was referred on chapter 2, the vault case of study is located on the Extreme West Body

basements of the Administration Building of the Hospital Sant Pau (Figure 6.1). It will be modelled a

quart of the total vault -one of the portions supported on the walls-, using symmetry boundary

conditions to simulate the whole structure (Figure 6.2).

The vault has double curvature, is much segmented and covers a quadrilateral surface of

8.8 m x 8.8 m, with only 9 cm of thinness. The vault is supported by walls on three of its edges and an

arch that separates the basement body, serving also as support to another vault with the same

characteristics. Within the walls and the arch, there is a metallic structure that absorbs the thrusts

generated by the vaults (Figure 6.2). As it is stated on the restoration works, the metallic elements are

IPN 100 and UPN 200, but for the vault portion chosen only the IPN are considered. The cross section

of this element is shown on Figure 6.3.

Figure 6.1 - Hospital Sant Pau: location of the vault case of study [ONL]

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Figure 6.2 - Vault plan with the portion analyzed shown in red [Jordi Bernuz].

Figure 6.3 - Model steel elements cross section (IPN-100)

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6.1.2 Mechanical properties

Due the characteristics of the tiles, and because there is no information about the compressive

strength, a value of 4 (MPa), is assumed. The Elastic Modulus is given by the equation E=500 fc,

which is an expression formulated by the UPC members based on the experience gained after years

of investigation and analysis on historical constructions. The tensile strength is taken as 5% of

compressive strength. Fractural energy is given by the concept of ductility index. The resulting values

are shown on Table 6-1.

Table 6-1 - Tile mechanical properties values

Value Units

Elastic Modulus E 2 GPaPoisson's ratio ν 0.22 -

Density ρ 1800 kg/m3

Compresion strength fc 4 MPa

Tensile Strenght ft 0.2 MPa

Fracture Energy Gf 50 N/m

Property

For steel, the values were estimated based on the type of steel used during the time of construction of

the hospital, and are shown on Table 6-2.

Table 6-2 - Steel mechanical properties values

Value Units

Elastic Modulus E 210 GPaPoisson's ratio ν 0.3 -

Density ρ 7850 kg/m3

Yield strength fy 250 MPa

Property

6.2 Model 1

6.2.1 Model Description

As a first approach, the vault was modelled as simply supported (no-rotation restriction). This was

done for verifying if the vault could stand without the help of additional elements. In order to avoid

stresses concentrations, the vault support was considered to be a linear element, instead of a single

point. The boundary conditions are shown on Figure 6.4. The structure was loaded by self-weight, and

it was incremented till failure was produced, so the failure load is represented as a percentage of the

structure self-weight.

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Figure 6.4 - Model 1: Boundary Conditions

6.2.2 Results

The maximum vertical deflection is 2.8 cm and occurs on the middle of the vault (Figure 6.5a, circled

on red). There is a uniform displacement with a tendency to deform against the gravity in the region

close to the support, and to do it on the opposite direction as it gets close to the middle of the vault

(Figure 6.5b).

(a)

(b)

Figure 6.5 - (a) vertical deflection, (b) Total deformed variation (amplified)

A load-displacement curve is drawn using as control point the node located on the middle of the vault,

in order to obtain a relation between the maximum load and the maximum displacement (Figure 6.6).

From this curve, it is observed that the failure of the structure takes place at only 43% of the self

weight, which means that the vault cannot be supported by itself.

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Figure 6.6 – Load-Displacement curve on the middle of the vault.

By analyzing the Maximum Principal Stress results of the vault upper surface (Figure 6.7a), there are

tensile stresses concentration on the middle of the vault edges and near the support surroundings, so

formation of hinges and cracks appearance are expected to occur on these points. After the hinges on

the middle of the edges are formed, the tensile stresses are spread to the interior of the vault,

concentrating there and generating a collapse zone that does not fully develops, meaning that the

cracks will propagate towards this area. On the vault bottom surface (Figure 6.7b) there is a great

zone near the support that bears a big amount of tensile stresses, becoming a hinge and generating a

collapse plane. This zone releases the tensile stresses concentration to the interior and to the edges

of the vault, as it cannot afford to support the entire load of the structure. The middle of the vault is

always on compression.

(a)

(b)

Figure 6.7 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

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With the Maximum Principal Strains results (Figure 6.8), it is clear that failure occurs due to tensile

stresses concentration on the vault bottom surface, on the zone close to the support, as there are

concentrated large deformations (Figure 6.8b). There are also important deformations on the middle

edges of the vault upper surface, but these are not that significant as the ones of the bottom surface.

The Crack Distribution results (Figure 6.9) also shows damage on almost all the vault bottom surface,

being the greatest one on the one close to the support.

(a)

(b)

Figure 6.8 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

(a)

(b)

Figure 6.9 - Crack Distribution (a) Top Surface, (b) Bottom Surface (Maximum in red, Minimum in

blue).

On the other hand, there does not seem to be a significant damage due to compression stresses, as it

can be observed on the Minimum Principal Stresses results (Figure 6.10), where the compression

values obtained are small in comparison with the material compressive strength.

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(a)

(b)

Figure 6.10 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

In conclusion, the collapse of the vault is due to the formation of a failure zone on the bottom surface

that acts as an internal support, not rigid and strong enough to bear the tensile stresses concentration

(because of the material mechanical properties), as a consequence of the incapacity of the supports to

take and distribute the load in an adequate manner, so it is advisable the use of external supports to

improve the behaviour of the vault.

6.3 Model 2

6.3.1 Model Description

This model was considered to be simply support (the same as model 1) but, in this case, modelling the

walls as boundary conditions restraining the vertical movement on the vault edges (Figure 6.11). The

structure was loaded by self-weight, and it was incremented till failure was produced, so the failure

load is represented as a percentage of the structure self-weight.

Figure 6.11 - Model 2: Boundary Conditions

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6.3.2 Results

The maximum vertical deflection is 2.25 cm and occurs on the middle of the vault (Figure 6.12a,

circled on red). There is a uniform displacement with a tendency to deform against the gravity in the

region close to the support, and to do it on the opposite direction as it gets close to the middle of the

vault (Figure 6.12b). Besides, the supports provided with boundary conditions restraining the vertical

displacement, causes the vault to stay without deformation on the edges but with a uniform

deformation on the rest of the surface, a non realistic solution due to the deformable nature of the real

walls supporting the vault (Figure 6.12c).

(a)

(b)

(c)

Figure 6.12- (a) vertical displacements, (b) Total deformed variation (amplified), (c) Total deformed

shape (amplified)

Figure 6.13 – Load-Displacement curve on the middle of the vault.

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A load-displacement curve is drawn using as control point the node located on the middle of the vault

in order to obtain a relation between the maximum load and the maximum displacement (Figure 6.13).

From this curve, it is observed that the failure of the structure takes place at only 66% of the self

weight, which means that the vault cannot be supported by itself.

By analyzing the Maximum Principal Stress results of the vault upper surface (Figure 6.14a), the

tensile stresses are spread through the vault edges, being mainly concentrated on the middle of this

boundaries, so cracks are expected to appear around the edges and hinges formation to occur on the

points of maximum concentration. On the vault bottom surface (Figure 6.14b), there is a tensile stress

concentration zone near the support, generated in a similar way that on model 1, but in this case, the

stresses are spread to the vertical supports in a more effective way. However, tensile stresses are

distributed all around the bottom surface, but they get finally concentrated again on the middle of the

edges so hinges formation are expected to occur on these points.

(a)

(b)

Figure 6.14 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

The Maximum Principal Strains results (Figure 6.15) shows better the deformed zones due to tensile

stresses concentration. On the vault upper surface (Figure 6.15a), the bigger deformations are on the

middle of the edges, so it is clear that these are zone with the highest tensile concentrations. On the

vault bottom surface (Figure 6.15b), there is a zone, between the middle of the vault and the support,

that presents high deformation, so it can be interpreted that tensile stresses started generating there

but were spread to the vault edges, to finally concentrate again on the middle of the edges, zones that

also exhibit high deformations.

The Crack Distribution results (Figure 6.16) shows, on the vault upper surface, big damage on the

zones surrounding the edges, while on bottom surface, the damage is distributed all over this face,

being higher on the zone between the middle of the vault and the support, and on the middle of the

edges.

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(a)

(b)

Figure 6.15 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

(a)

(b)

Figure 6.16 - Crack Distribution (a) Top Surface, (b) Bottom Surface (Maximum in red, Minimum in

blue).

(a)

(b)

Figure 6.17 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

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On the other hand, there does not seem to be a significant damage due to compression stresses, as it

can be observed on the Minimum Principal Stresses results (Figure 6.17). There is a low concentration

of compressive stresses close to the support, but the rest of the structure supporting compressive

values very small in comparison with the material compressive strength. ´

In conclusion, the collapse of the structure results from the formation of hinges on the middle of the

vault edges due to tensile stresses concentration, phenomenon that occurs because the vertical

supports are not good enough to counteract the stresses generated, and there is not any additional

support on the system that helps to release and redistributed them to another areas, so a mechanism

that helps to allocate the stresses must be implemented.

6.4 Model 3

6.4.1 Model Description

For this model the support restrains only the vertical movement, while the horizontal ones are

restrained by two beam elements placed to simulate the action of the hidden metallic structure (Figure

6.19). Because these elements are modelled as single beams, and there two IPN-100 steel elements

on the existing structure, the cross section of the beam elements was considered to be the double

(Figure 6.18). The mechanical properties of the mesh elements affected by the beam elements

stiffness was changed for elastically ones, so the stresses concentration do not influence the failure of

the structure.

The vault has boundary conditions restraining the vertical movement in all the edges. The steel

elements have a displacement restriction on their parallel direction and rotation restrictions on the

perpendicular directions in order to simulate symmetry properties. The structure was loaded by self-

weight, and it was incremented till failure was produced, so the failure load is represented as a

percentage of the structure self-weight.

Figure 6.18 - Proportional steel cross-section

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Figure 6.19 - Model 3: Boundary Conditions

6.4.2 Results

The maximum vertical deflection is 6.5 cm and occurs on the middle of the vault (Figure 6.20a, circled

on red). The behaviour observed is very similar to the one observed on model 2, but in this case, the

deflection is bigger due to the addition of material with elastic mechanical properties (Figure 6.20b).

The deformation of the beam elements seems to be high due to the amplification of the image, but the

deformation values obtained are below the millimetres (Figure 6.20c)..

(a)

(b)

(c)

Figure 6.20- (a) vertical displacements, (b) Total deformed variation (amplified), (c) Total deformed

shape (amplified)

A load-displacement curve is drawn using as control point the node located on the middle of the vault

in order to obtain the relation between the maximum load and the maximum displacement (Figure

6.21). From this curve, it is observed that the failure of the structure takes place at 104% of the self

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weight, which means that the vault can stand its own eight but fails when this is increased by an

additional 4%. Also, there is a change on the structural behaviour of the vault –with respect on the

previous models-, as the graphic obtained has similarities with the behaviour of elastic structures,

behaviour that seems to be influenced by the addition of the steel. An increase on the deformation

without any apparent load increase is appreciated between the 5 cm and 6 cm, incident that denotes

the use of materials with different elastic properties

Figure 6.21 - Load-Displacement curve on the middle of the vault.

By analyzing the Maximum Principal Stress results of the vault upper surface (Figure 6.22a), the

tensile stresses are originated on a zone between the support and the middle of the vault, and are

spread towards the vault edges, being mainly concentrated on the middle of this boundaries, so

cracks are presumed to appear on the tensile stresses concentration zone and around the edges,

while hinges formation are expected to occur on the middle of the vault edges. On the vault bottom

surface (Figure 6.22b), the tensile stresses are concentrate on the same zone as on the upper

surface, but these are spread on almost all the surface, except the middle of the vault that bears

compression stresses. The spread path followed for dissipating the tensile stresses generated throw

the steel elements is noticeable. Anyway, they do not distribute well all the stresses, so the failure is

produced again on the middle of the vault edges after a low load portion is applied, where hinges are

expected to appear. The influence of the steel elements stiffness is observed by the tensile stresses

concentration on the mesh elements surrounding the support.

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The Maximum Principal Strains results (Figure 6.23) shows, on the upper vault surface, the hinges

formed due to tensile stresses concentration –on the middle of the edges-, while on the vault bottom

surface, is evident the big deformation produced on the zone between the middle of the vault and the

support. Also, these results help to clarify the path followed by the tensile stresses and the

development of the failure (Figure 6.23b). The Crack Distribution results (Figure 6.24) show the same

behaviour.

(a)

(b)

Figure 6.22 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

The Maximum Principal Strains results (Figure 6.23),show, on the upper surface, the hinges formed

due to tensile stresses concentrations, being large deformation on the middle of the edge arches,

while on the bottom surface is evident the tensile stresses concentrates between the middle of the

vault and the support. Also, these results help to clarify the path followed by the stresses and the

development of the failure. The Crack Distribution results (Figure 6.24) show the same behaviour and

shows clearly the hinges expected to be formed.

(a)

(b)

Figure 6.23 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

As opposite to all previous models, the Minimum Principal Stresses results show bigger values (Figure

6.25), especially on the zone between the vertical support and the middle of the vault, evidencing the

high compressive stresses concentration develop on this zone but do not constitute a big risk to the

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structure resistance because the values obtained are small in comparison to the material compressive

strength. The corners of the vertical supports also shows big concentrations, but this is due to the

effect of the steel element stiffness.

(a)

(b)

Figure 6.24 - Crack Distribution (a) Top Surface, (b) Bottom Surface (Maximum in red, Minimum in

blue).

(a)

(b)

Figure 6.25 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

The collapse of the vault occurs in a similar way as on model 2, with the difference that, for this case,

the stresses are better distributed along the vault surface due to the implementation of a mechanism

that bears part of the thrusts produced, but not efficient enough for dissipating the stresses generated

properly, so these are faster concentrated on the zones previously exposed, generating the failure of

the system.

6.5 Model 4

6.5.1 Model Description

The vault was considered to be simply supported, with boundary conditions on the edges restraining

vertical and horizontal movements, simulating the actions of walls and metallic structure respectively.

The structure was loaded by self-weight, and it was incremented till failure was produced, so the

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failure load is represented as a percentage of the structure self-weight. The model is shown on Figure

6.26.

Figure 6.26 - Model 4: Boundary Conditions

6.5.2 Results

The maximum vertical deflection is 5.7 cm and occurs on the middle of the vault (Figure 6.27a, circled

on red). It is observed that there are minor or no displacements on the zone influenced by the vertical

and horizontal constrains, but it starts to deform uniformly after this influence is surpassed (Figure

6.27b).

(a)

(b)

Figure 6.27 - (a) vertical displacements, (b) Total deformed variation (amplified)

A load-displacement curve is drawn using as control point the node located on the middle of the vault

in order to obtain the relation between the maximum load and the maximum displacement (Figure

6.28). From this curve, it is observed that the structure failure takes place at 250% of the self weight, a

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big value in comparison with the ones obtained on previous models. Besides, the curve shows an

ideal behaviour as it has not leaps or variation.

Figure 6.28 - Load-Displacement curve on the middle of the vault.

By analyzing the Maximum Principal Stresses results of the vault upper surface (Figure 6.29a), it is

observed that the vault resists principally, compressive stresses, and the zones having tensile

stresses concentrations are the ones located on the middle of the vault edges. The same applies for

the Maximum Principal Stresses on the bottom surface (Figure 6.29b), where the tensile stresses

concentrations appears on the same zone. It can be seen that the centre of the vault resist the highest

compression stresses and these are uniformly distributed throw the entire surface, which means that

the stresses generated on the centre of the vault are easily spread to the vault edges –which are

constrained for vertical and horizontal movement-, and are finally concentrated on the middle of this

zones, where tensile stresses are generated, favouring hinges appearance and causing the structure

to fail.

The Maximum Principal Strains results (Figure 6.30) shows deformation due to compression stresses

on the middle of the vault while big deformations on the middle of the vault edges due to tensile

stresses. On the Crack Propagation results (Figure 6.31), the damage is localized on the middle of the

vault edge, for both upper and bottom surface. The Minimum Principal Stresses results show bigger

values of compression than on the previous models, but these are small compared to the material

compressive strength (Figure 6.32).

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(a)

(b)

Figure 6.29 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

(a)

(b)

Figure 6.30 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

(a)

(b)

Figure 6.31 - Crack Distribution (a) Top Surface, (b) Bottom Surface (Maximum in red, Minimum in

blue).

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(a)

(b)

Figure 6.32 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

In Conclusion, the behaviour observed corresponds to the one expected for a vault: compression on

almost the entire surface of the vault with tensile stresses concentrations forming hinges on the middle

of the edges. However, the boundary conditions implemented makes the vault to behave very different

from the existing one, since the results shows an idealised behaviour -something very difficult to

achieve on reality-, so the model serves to understand the theoretical vault collapse mechanism but

no to represent the system and the causes of failure.

6.6 Model 5

6.6.1 Model Description

For this case the supporting walls are also modelled so the support and the boundary conditions

restraining the vertical movement used on previous models were eliminated. The only boundary

conditions taken into account are the ones representing the vault symmetry (Figure 6.33).

Figure 6.33 - Model 5: Boundary Conditions

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The structure was loaded by self-weight, and it was incremented till failure was produced, so the

failure load is represented as a percentage of the structure self-weight. Because the load obtained

exceeded the self-weight, a second approach was done by loading the system with 100% of its self-

weight and applying proportionally load increments by factors of a distributed force of 4000 N/m2 over

the vault surface till failure was achieved.

6.6.2 Results

The maximum vertical deflection is 3.0 cm and occurs on the middle of the vault (Figure 6.34a, circled

on red). It is observed that there are minor or no displacements on the zone influenced by the walls,

being practically nullified near the corner -where the two perpendicular walls are joined- but it starts to

deform uniformly towards the middle of the vault after this influence is surpassed (Figure 6.34b).

(a)

(b)

Figure 6.34 - (a) vertical displacements, (b) Total deformed variation (amplified)

Figure 6.35 – Load-Displacement curve at the middle of the vault as a factor of self weight.

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Figure 6.36 – Load-Displacement curve on the middle of the vault.

A load-displacement curve is drawn using as control point the node located on the middle of the vault

in order to obtain the relation between the maximum load and the maximum displacement (Figure

6.35). From this curve, it is observed that the failure of the structure takes place at 122%, which

means that it supports its self-weight plus an additional increment of 22%.

A second load-displacement curve is shown but with values of a distributed load over the vault surface

after the self-weight has been applied, obtaining as load failure 408 N/m2 (Figure 6.36).

(a)

(b)

Figure 6.37 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

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By analyzing the Maximum Principal Stresses results of the vault upper surface (Figure 6.29a), the

stresses are spread from the middle of the vault to its edges –where the walls are located-, getting

concentrated on the middle of these, generating a tensile stresses concentration zone similar as

previous models; hinges are expected to form on these zones. Also, Maximum Principal Stresses on

the vault bottom surface presents the same behaviour as previous models: tensile stresses starts

concentrated on a zone between the middle of the vault and the union of the perpendicular walls and

are spread to the edges where they get concentrated on the middle, favouring hinges appearance and

causing the structure to fail.

(a)

(b)

Figure 6.38 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

(a)

(b)

Figure 6.39 - Crack Distribution (a) Top Surface, (b) Bottom Surface (Maximum in red, Minimum in

blue).

The Maximum Principals Strains show basically the deformation caused by the tensile stresses

propagation throw the walls (Figure 6.38). If these results are analyzed in combination with the Crack

Propagation results (Figure 6.39), it can be observed damage on the edges, where the union between

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the vault and the walls takes place, probably due to crushing of the bonded elements because the

interaction of these structures is modelled as a union between two rigid materials, without using

interface elements. However, the damage distribution is similar to the one observed on previous

models, so this effect does not seem to affect the overall behaviour of the structure, but can influence,

negatively, the load capacity of the vault.

As it was expected, there does not seem to be a significant damage due to compression stresses, and

the values obtained for the Minimum Principal Stresses are very small compared to the material

compressive strength (Figure 6.40). It is appreciable that the centre of the vault bears the biggest

compressive stresses.

(a)

(b)

Figure 6.40 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

The behaviour and the failure of this model are very similar to the ones obtained with the previous

models: tensile stresses concentrations on the middle of the edges after they are propagated throw

the walls. The crushing produced by the interaction between the walls and the vault does not seem to

affect the structural behaviour, but they influence the vault capacity results.

The load capacity value obtained for this model is enough for a vault serving as a ceiling, supporting

its self-weight and periodically addition of loads due to maintenance, but not for serving as a

dependency of the hospital, so the model must be improved.

6.7 Model 6

6.7.1 Model Description

This model has the same characteristics as model 5 but with the addition of beam elements

representing the metallic structure hidden on the walls. As it was done on model 3, the mechanical

properties of the mesh elements affected by the steel stiffness were changed for elastic ones. Also,

the cross-section is the same used for the beam elements on model 3. The boundary conditions of the

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model are shown on Figure 6.41. The beam elements are shown in yellow while the elastic elements

are shown in green. The vault is also shown in yellow while the walls are on red.

Figure 6.41 – Model 6: Boundary Conditions

The structure was loaded by self-weight, and it was incremented till failure was produced, so the

failure load is represented as a percentage of the structure self-weight. Because the load obtained

exceeded the self-weight, a second approach was done by loading the system with 100% of its self-

weight and applying proportionally load increments by factors of a distributed force of 4000 N/m2 over

the vault surface till failure was achieved.

6.7.2 Results

The maximum vertical deflection is 5.8 cm and occurs on the middle of the vault (Figure 6.42a, circled

on red). As on model 5, there deformation is uniform, being higher on the middle of the vault and

minimum on the union of the perpendicular walls, where it practically nullifies due to the influence of

the supporting walls (Figure 6.42b.

(a)

(b)

Figure 6.42 - (a) vertical displacements, (b) Total deformed variation (amplified)

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A load-displacement curve is drawn using as control point the node located on the middle of the vault

in order to obtain the relation between the maximum load and the maximum displacement (Figure

6.43). From this curve, it is observed that the failure of the structure takes place at 169%, which

means that it supports its self-weight plus an additional increment of 69%.

A second load-displacement curve is shown but with values of a distributed load over the vault surface

after the self-weight has been applied, obtaining as load failure 932 N/m2 (Figure 6.44).

Figure 6.43 – Load-Displacement curve on the middle of the vault as a factor of self weight.

Figure 6.44 – Load-Displacement curve on the middle of the vault.

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(a)

(b)

Figure 6.45 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

By analyzing the Maximum Principal Stresses results of the vault upper surface (Figure 6.45a), it is

evident that the stresses distribution is similar to the ones obtained on model 5: tensile stresses

concentration on the vault edges, with higher amounts on the middle that propitiates the formation of

hinges. The only difference with model 5 is the concentration of tensile stresses on the corner of the

vaults –where the perpendicular walls are join-, due to the steel elements presence which takes part of

the stresses generated over the vault surface (Figure 6.45b). The same applies for the Maximum

Principal Stresses results of the vault bottom surface, presenting a similar behaviour to model 5, but

with a decrease on the tensile stresses concentration on the zone where the steel elements are set.

(a)

(b)

Figure 6.46 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

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The Maximum Principals Strains shows the same behaviour than model 5, and the zones with more

deformations are evident (Figure 6.46). The Crack Propagation results (Figure 6.47) shows also a

better distribution of the damage through the vault than on model 5 due to the contribution of the steel

elements to the structural performance of the vault. Again, hinges are formed on the middle of the

vault edges.

(a)

(b)

Figure 6.47 - Crack Distribution (a) Top Surface, (b) Bottom Surface (Maximum in red, Minimum in

blue).

The Minimum Principal Stresses results show an increment of the compression values on the vault

surface –especially on the upper surface- but, as it was expected, these are small in comparison to

the material compressive strength (Figure 6.48).

(a)

(b)

Figure 6.48 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

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By the addition of the steel elements, the behaviour of the structure is improved. However the final

load resisted is not good enough for services purposes, so the model needs to be checked again for

increasing its capacity. The failure mode, as well as the hinges developed, is produced in the same

way as on previous models: tensile stresses concentration on the middle of the vault edges.

6.8 Model 7

6.8.1 Model Description

This model is basically the same as model 6 but with the addition of the floor supporting ribs; these

elements are placed over the vault surface, acting as braces and increasing its stiffness. They were

considered to be spaced every 50 cm and with 15 cm of thickness (Figure 6.49a). The model is shown

on Figure 6.49b, with the steel elements on red while the elastic ones are shown in light yellow; the

ribs are shown on a darker yellow.

The structure was loaded by self-weight, and it was incremented till failure was produced, so the

failure load is represented as a percentage of the structure self-weight. Because the load obtained

exceeded the self-weight, a second approach was done by loading the system with 100% of its self-

weight and applying proportionally load increments by factors of a distributed force of 4000 N/m2 over

the vault surface till failure was achieved.

(a)

(b)

Figure 6.49 – (a) Ribs, (b) Model 7: Boundary Conditions.

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6.8.2 Results

The maximum vertical deflection is 9.71 cm and occurs on the middle of the vault (Figure 6.50a,

circled on red). It is observed that there are minor or no displacements on the zone influenced by the

walls, being practically nullified near the corner -where the two perpendicular walls are joined- but it

starts to deform uniformly towards the middle of the vault after this influence is surpassed. (Figure

6.50b). The deformation is not symmetrical, and it tends to be higher on the unbraced direction.

(a)

(b)

Figure 6.50 - (a) vertical displacements, (b) Total deformed variation (amplified)

Figure 6.51 – Load-Displacement curve at the middle of the vault as a factor of self weight.

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Figure 6.52 – Load-Displacement curve at the middle of the vault.

A load-displacement curve is drawn using as control point the node located on the middle of the vault

in order to obtain the relation between the maximum load and the maximum displacement (Figure

6.51). From this curve, it is observed that the failure of the structure takes place at 206%, so the

structure supports its self-weight two times. A second load-displacement curve is shown but with

values of a distributed load over the vault surface after the self-weight has been applied, obtaining as

load failure 2748 N/m2, a considerable high value (Figure 6.52).

By analyzing the Maximum Principal Stress results of the upper vault surface (Figure 6.53a), there are

tensile stresses concentrated uniformly all over the surface of the vault, and seems to be generated,

mainly, by the action of the ribs; these have a tendency to concentrate on the perpendicular direction

of the ribs, which is the unbraced direction. The zone affected by the presence of the steel elements

has less tensile stresses concentrations, as these takes part of the stresses generated over the vault

surface; the ribs allows the vault to work more efficiently, as there are not isolated zones with high

tensile stresses concentration. Even if the highest tensile stresses values are located around the

middle of the vault edges, it is evident that damage is produced all over the vault upper surface

On the bottom surface (Figure 6.53b), tensile stresses starts concentrating at the end of the ribs,

principally on the connections with the walls and are distributed through them by following the ribs

directions. It can also be observed that the middle of the vault resist compressive stresses.

The Maximum Principals Strains show basically the tensile stresses path propagation through the

walls (Figure 6.54), where there are high deformations on the union between the walls and the vault

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-due to the crushing effect mentioned on the results of model 6-, being majorly concentrated on the

zones close to the vault middle edges. The Crack Distribution results show also great damage all over

the surface of the vault with the highest damage located near the middle of the vault edges (Figure

6.55).

(a)

(b)

Figure 6.53 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

(a)

(b)

Figure 6.54 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

The Minimum Principal Stresses results over the top surface shows big compressive stresses

concentration due to the actions of the ribs acting over the surface, being higher near the wall unions,

but decreasing on the distance, being minimum on the middle of the vault (Figure 6.56a). On the

bottom surface, the highest values are on the middle of the vault (Figure 6.56b). In both results, the

values obtained are relatively small in comparison to the material compressive strength.

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(a)

(b)

Figure 6.55 - Crack Distribution (a) Top Surface, (b) Bottom Surface (Maximum in red, Minimum in

blue).

(a)

(b)

Figure 6.56 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

By adding the ribs, the model shows a better structural behaviour than the previous ones: the stresses

are uniformly distributed all over the vault surface. Also, there is a considerable increase on the vault

capacity load, which means that the vault resist the service purposes for it was conceived. However,

the vertical deflection value obtained is too high to be considered a satisfactory solution.

6.9 Model 8

6.9.1 Model Description

The model is basically the same as model 7, but with the beams elements modelled as a simplification

of the existing metallic structure. The real structure is shown on Figure 6.57a while the model

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simplification is on Figure 6.57b. The resulting model is shown on Figure 6.58, with the steel elements

on blue, the vault and the walls on green and the ribs and the walls containing the steel elements on

yellow.

The structure was loaded by self-weight, and it was incremented till failure was produced, so the

failure load is represented as a percentage of the structure self-weight. Because the load obtained

exceeded the self-weight, a second approach was done by loading the system with 100% of its self-

weight and applying proportionally load increments by factors of a distributed force of 4000 N/m2 over

the vault surface till failure was achieved.

(a)

(b)

Figure 6.57 - Metallic structure (a) existing [González et. al., 2011], (b) Model simplification.

Figure 6.58 - Model 8: Boundary Conditions

6.9.2 Results

The maximum vertical deflection is 4.8 cm and occurs on the middle of the vault (Figure 6.59a, circled

on red). It is observed the same behaviour as on model 7: there are minor or no displacements on the

zone influenced by the walls, deforming uniformly towards the middle of the vault, with an

asymmetrical deformation, having higher values on the unbraced direction (Figure 6.59b).

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(a)

(b)

Figure 6.59 - (a) vertical displacements, (b) Total deformed variation (amplified)

Figure 6.60 - Capacity curve at the middle of the vault as a factor of self weight.

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Figure 6.61 - Capacity curve at the middle of the vault.

A load-displacement curve is drawn using as control point the node located on the middle of the vault

in order to obtain the relation between the maximum load and the maximum displacement (Figure

6.60). From this curve, it is observed that the failure of the structure takes place at 201%, so the

structure supports its self-weight two times. There is an increase of the deformation without any

apparent load increment due to the use of mesh elements with elastic properties on the zones affected

by the steel stiffness. A second load-displacement curve is shown but with values of a distributed load

over the vault surface after the self-weight has been applied, obtaining as load failure 2800 N/m2,

value slightly above the one obtained on model 7, but in this case with a lower deformation (Figure

6.61).

By analyzing the Maximum Principal Stress result s of the upper vault surface (Figure 6.62a), it is

observed the same behaviour obtained with model 7: tensile stresses concentrated uniformly all over

the surface of the vault generated by the action of the ribs with a tendency to concentrate on the

perpendicular direction of the ribs, which is the unbraced direction; the influence of the steel elements

taken the stresses concentrated between the two walls. The only main difference is that, in this case,

the stresses concentrate more on the middle of the unbraced edge, so a hinge is produced on this

zone.

As in model 7, tensile stresses the bottom surface (Figure 6.62b) start generating on the connections

of the ribs with the walls, but also on the wall that is not connected to the ribs. The zone with more

concentrations is the middle edge of the braced direction.

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(a)

(b)

Figure 6.62 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

By analyzing the Maximum Principal Stress results of the upper surface of the vault (Figure 6.62a), it is

observed the same stresses distribution obtained with model 7: tensile stresses concentrated

uniformly all over the vault surface, generated by the action of the ribs with a tendency to concentrate

perpendicularly to the ribs direction -which is the unbraced direction-; and the steel elements helping

to dissipate stresses concentrations on the vault surface The only main difference is that, in this case,

the stresses concentrate more on the middle of the unbraced vault edge, so a hinge is expected to

form on this zone. As in model 7, on the vault bottom surface (Figure 6.62b), tensile stresses starts

generating on the connections of the ribs with the walls and on the unbraced zones.

(a)

(b)

Figure 6.63 - Maximum Principal Strains (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

The Maximum Principals Strains results (Figure 6.63).show basically big deformations on the

connections of the ribs with the walls. The concentration of deformations between the walls and the

vault is due to the crushing phenomenon already described. The Crack Propagation results (Figure

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6.64) show also damage on almost all the vault surface, being mainly concentrated on the ribs; the

highest damages are produced on the zone located on the middle of one of the vault edges –the one

on the braced direction-, so it is supposed that the failure is produced at this point.

The Minimum Principal Stresses results of vault upper surface shows high compression stresses

concentrations due to the actions of the ribs acting over the vault surface (Figure 6.65a). On the

bottom surface, the highest values seem to be on the middle of the vault (Figure 6.65b). As it was

expected, the values obtained are relatively small in comparison to the material compressive strength.

(a)

(b)

Figure 6.64 - Crack Distribution (a) Top Surface, (b) Bottom Surface (Maximum in red, Minimum in

blue).

(a)

(b)

Figure 6.65 – Minimum Principal stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

By modelling the metallic structure in a similar way as the existing one, the model shows a better

structural behaviour than the previous ones by having uniformly stresses distribution all over the vault

surfaces, and a considerable high increment on the resistant load with a low deflection value. Damage

is distributed all over the upper vault surface by tensile stresses concentration, being the first zone to

fail the middle of the vault edge located on the brace direction.

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6.10 Model Comparison

On Figure 6.66 is shown the load-displacement curve on the middle of the vault for all the models, with

the load represented as a factor of the self-weight. The models present, in general, a similar

behaviour. The models where boundary conditions were used to simulate the effect of the walls and

the metallic structure, shows softer curves, which means that they behave in an idealized way

(Model 1, Model 2, Model 3 and Model 4). However, the behaviour of the structure is better

understood when all the elements are modelled (Model 5, Model 6, Model 7 and Model 8).

Figure 6.66 – Load-Displacement curve on the middle of the vault as a factor of self weight for all

models.

Model 4 shows the most idealized behaviour of the structure and even if with this model the maximum

load factor is reached, it does not represent properly the structural system behaviour. For example,

the effect that the steel elements and the ribs have on the vault behaviour is not appreciable on the

curve.

The load-displacement curves of the models with metallic structure incorporated (Model 2, Model 3,

Model 5, Model 6 and Model 7) shows a lapse in which the deformation increase without any apparent

load increment. By modelling the metallic structure as the existing one (Model 8), the mentioned lapse

practically disappears, and the resultant curve is different from all the models; it can be concluded that

the hidden metallic structure serves not only to counteract the vault thrusts but to stiff it, so the vault

deformation decreases (the deformation at the end of this curve is due to the influence of the elastic

elements).

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On Figure 6.67 is shown the load-displacement curves on the middle of the vault obtained by the

action of the distributed load -not as a self-weight factor- for the models where the walls were

modelled. The results show the same curvature tendency for these models and the increase of the

load capacity as they are improved. It is appreciable how the stiffness obtained for model 8 differs

from the rest of the models, effect only understandable by the presence of the metallic structure.

Figure 6.67 – Load-Displacement curve at the middle of the vault for the models.

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7 PARAMETRICAL ANALYSIS

A brief parametric analysis is performed in order to evaluate the response of the model to variations

on the Compressive Strength and the Fracture Energy. Model 8 was chosen for this study, as it was

the one with the best overall behaviour. The values used for compressive strength were 1 MPa and

2 MPa, and the results were compared with the ones obtained for the standard model with fc = 4 Mpa.

For the Fracture Energy, the values were 25 N/m and 100 N/m, and the results were compared with

the values obtained on the standard model with Gf = 50 N/m.

7.1 Compressive strength

7.1.1 fc = 1 MPa

For the model with fc = 1 MPa, the load capacity obtained was 2208 N/m2 (Figure 7.1), a lowered value

compared with the standard model. Also, the resultant behaviour is slightly different, as the stiffness of

the structure decreases. For the Maximum Principal Stresses results, it is observed that the tensile

stresses concentration diminish (Figure 7.2) in comparison to the ones obtained on Chapter 6.9.2

(Figure 6.62).

Figure 7.1 – Load-Displacement curve at the middle of the vault for fc = 1 MPa

On the other hand, the Minimum Principal Stresses increase and are distributed all over the vault

surface. On the vault upper surface, there are compressive stresses concentrations on the zone near

the walls connection -the unbraced space- (Figure 7.3a). On the bottom surface (Figure 7.3b), these

are concentrated mainly on the middle of the vault.

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(a)

(b)

Figure 7.2 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

(a)

(b)

Figure 7.3 - Minimum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

(a)

(b)

Figure 7.4 – Crack Distribution (a) Top Surface, (b) Bottom Surface (Maximum in red, Minimum in

blue).

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However, the model fails by punctual tensile stresses concentration on the union of the walls and the

ribs (Figure 7.4), but due to the amount of stresses concentration generated by compression, it is

more feasible that failure will occur by crushing of the central part of the vault and the zone influenced

by the walls connection.

7.1.2 fc = 2 MPa

For the model with fc = 2 MPa, the load capacity was 2716 N/m2 (Figure 7.5), a slightly decrease

compared to the standard model but with a deformation of 5.3 cm, a significantly higher value (see

Chapter 6.9.2). For the Maximum Principal Stresses results, the same behaviour as the model with

fc = 1 MPa is obtained, but there is a reduction on the tensile stresses concentration over the vault

surface.

Figure 7.5 – Load-Displacement curve on the middle of the vault for fc = 2 MPa

(a)

(b)

Figure 7.6 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

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By analyzing the Minimum Principal Stresses on the vault upper surface, there are compression

stresses concentrated mainly on the zone closed to the walls connection union, and is not as high like

it was for the model with fc = 1 MPa (Figure 7.3a). On the bottom surface these do not have a great

concentration likely to produce a failure of the structure (Figure 7.3b).

(a)

(b)

Figure 7.7 - Minimum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

By this, the failure mechanism is produced by compressive stresses concentration on the unbraced

zone influenced by the walls connection.

7.1.3 Compressive strength comparison

Figure 7.8 - Compressive strength load-displacement curve comparison

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As can be seen on Figure 7.8, the load-capacity values obtained have not a significant variation,

especially when the value is changed from 4 MPa to 2 MPa, where the appreciable difference is on

the final deformation. The final load supported by the model with fc = 1 MPa, is not considerably

different from the one obtained from standard model, if it is considered that the compressive strength

was reduced 4 times. By this, there no seems to be a great variation on the structure capacity when

the compressive strength is changed, but it affects the failure mechanisms and the structure

behaviour.

7.2 Fracture Energy

7.2.1 Gf = 25 N/m

For the model with Gf = 25 N/m, the load-capacity obtained was 1652 N/m2 (Figure 7.9) a considerable

low value compared to the one obtained for the standard model. However, there are not significant

changes on the structural performance. The deformation at the end of the curve, where there is not an

appreciable load increment, is due to the use of mesh elements with elastic properties on the zones

affected by the steel stiffness, so the final deformation is 3.3 cm, so it decreases in comparison with

the standard model.

Figure 7.9 – Load-Displacement curve on the middle of the vault for Gf = 25 N/m

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For the Maximum Principal Stresses results (Figure 7.10), the distribution of the stresses is practically

the same as the standard model, with the difference that the tensile stresses generated are not well

distributed in this case, and they are mainly concentrated on punctual points, so the failure is

produced on these points (see Chapter 6.9.2, Figure 6.62).

(a)

(b)

Figure 7.10 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

7.2.2 Gf = 100 N/m

By increasing the fracture energy to Gf = 100 N/m, the load-capacity obtained is 3932 N/m2, a

considerable high value if compared to the standard model (Figure 7.11); the final deformation is

6.3 cm, which is also bigger. The structural behaviour obtained has the same tendency as the

standard model, but the curves are softer and with basically only two changes on the curvature slope.

Figure 7.11 – Load-Displacement curve on the middle of the vault for Gf = 100 N/m

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(a)

(b)

Figure 7.12 - Maximum Principal Stresses (a) Top Surface, (b) Bottom Surface (Maximum in red,

Minimum in blue).

As previous model, the Maximum Principal Stresses results shows practically the same distribution of

tensile stresses as on the standard model, but with higher amounts of tensile stresses concentrated

over the vault surface in this case. Also, the failure obtained is the same as on the standard model.

7.2.3 Fracture energy comparison

Figure 7.13 – Fracture Energy load-displacement curve comparison

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As can be seen on Figure 7.13, the Fracture Energy is a parameter very sensitive to variations, and it

affects considerably the structure capacity. However, the same failure mechanism was observed for all

the cases analysed, so variations on this parameter do not apparently affect the overall structural

behaviour, but only is capacity.

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8 CONCLUSIONS

At present, there is not a standardized procedure for assessing the structural behaviour of timbrel

vaults. The most used method for evaluating the stability of these constructions, and the one that best

represents their behaviour is the limit analysis, but it is considered to be a restricted method for

performing the structural evaluation in 2D. Although FE models have been employed for representing

the structures in 3D, the problems derived from boundary conditions sensibility and input data has led

some authors to consider the use of these models inappropriate. On the other hand, the TNA method

proposed by Block [Block, 2009] has gained recognition due to fact that it solves the two main

difficulties of both limit analysis and FEM methods, and it should be included as an alternative for the

assessment of timbrel constructions.

For simulating the behaviour of one of the vaults located on the Administration building of the Hospital

Sant Pau, a FE model was elaborated. During the model development process it was proven that, in

order to obtain better results, the structure must be modelled by representing all its existing

components as real as possible and not simplifying them; in other words, avoiding the use of boundary

conditions instead of explicitly modelling the supporting elements.

Although the type of failure obtained for all the models was very similar and was the expected one,

formation of hinges on the vault edge points of maximum rise caused by the tensile stresses

concentration while the center of the vault bears compression stresses, the final overall behaviour for

all of the models was different.

The verifications performed on the vault demonstrate that it has the capacity to support, at least,

2800 N/m2. However, it is necessary to conduct some tests on the materials for calibrating the model

with the real mechanical properties values and improve the results. Additionally, in order to accept this

load-capacity value, it is advisable to carry out a load test so the results can be compared with the

ones obtained by the FEM.

The interaction between the wall and the vault was expected to behave as one rigid body. Even

though, this behaviour was not seen on the results. The model could be improved by using interface

elements between the two structures so the interaction between them is represented as one structure

with similar mechanical properties. With this improvement, the behaviour of one influences the other

and they do not act as independent bodies, thus avoiding the crushing of the connection zones.

It is more than probable that the final results obtained with a complete model –like displacements and

load failure- would have some variations, but the model generated represents in a good manner the

behaviour of the timbrel vault and provides an appropriate assessment about the stability and

resistance capacity of the vault.

With this model it was perceived the efficacy of the hidden steel elements implemented by Domènech

on the structural performance of the vault, which not only bears the horizontal thrusts generated but

stiffens the whole system, reducing the vault deformations and improving its structural behaviour.

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By the parametrical analysis, it was able to verify that changes on the compression strength properties

of the model do not alter significantly the load failure values but the structural behaviour of the vault;

the failure mechanism of the structure was different on the three cases analysed. On the other hand,

variations on the fracture energy properties alter significantly the structure resistance capacity but not

its structural performance so the same failure mechanisms were obtained for the three models.

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