glass structures
TRANSCRIPT
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ADVANCED DESIGN OF GLASS
STRUCTURES Lecture L1_ME
Design of glass beams
Martina Eliášová
European Erasmus Mundus Master Course
Sustainable Constructions
under Natural Hazards and Catastrophic Events520121-1-2011-1-CZ-ERA MUNDUS-EMMC
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Objectives of the lectureObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
• Introduction• Experimental research
• Elements subjected to bendings
• Lateral torsional buckling
• Design methods
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Museum of glass - Kingwindford, United Kingdom
• structure of extension: length 11,0 m
• distance 1,1 m
• height of column 3,5 m, depth 200 mm
• span of beam 5,7 m, depth 300 mm
• columns, beams – laminated
glass• snow load 0,75kN/m2
• roof, walls: insulated glass
units
Composition of insulated units:
• outer layer 10 mm float colourlesssolar-control glass
• cavity between the panels 10 mm
• inner layer: 2 x 6 mm of toughenedsafety glass with striped pattern of
baked-on ceramic ink
Practical examplesObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Connection between beam and
column
• three layered glass 3 x 10 mm
• bonded on site with casting resin – total thickness 32mm
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Eating room – family house in
London, UKBackdoor to the family
house - Germany
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Canopies – Nijmegen, Netherlands 1999
Cross section
1 – clamped steel column HEB300
2 – horizontal steel beam HEA300
3 – continuous glass beam – 3x10mm, float glass
4 – glass roof panels – 2x 10mm,
float glass
5 – vertical glass panel in gutter
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Glass canopy at the underground station – Tokyo, Japan
1996
• built-up beam
• size 10,6 x 4,8 m
• height 4,8 m
• length of cantilever 9 m• beam composed from
triangular fins
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Glass canopy at the underground station – Tokyo, Japan
1996
• panes with length 1,9 – 2,5 m
• toughened glass 2x 15 mm
• triangular fins (laminated glass 2x19 mm + acryl pane 40mm)
• acryl panes sufficient capacity incase of earthquake
• from 1 at top to 4 fins at supportwith respect to the bending
moment
• bolted connection
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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• span of main beams 14m indistance 2,7m; beams
composed of 13 fins withlength 4,5m – outer fins 2x
12mm, inner 10+19+10mm
• secondary beams in adistance 2,2m
primary
beams
secondarybeams
Glass roof of interior courtyard, commercial building in
Munich, Germany 2003
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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ELEMENTS SUBJETED TO BENDING
Glass roof of interior courtyard, commercial building in
Munich, Germany 2003
• secondary beams 2x 10mm, heatstrengthened glass
• bolted connection subjected by the
shear and bearing• roof – double insulated units (2,7 x
2,3m)
• high degree of precision – assembly
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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glass roof above interior
courtyard 24 x 30m
Glass roof for refectory at the TU Dresden, Germany 2006
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Glass roof for refectory at the TU Dresden, 2006
• span of the principal beams5,75m
• secondary beams indistance of 1,45m
• beams depth 350mm, 4x12mm fully tempered glass
installation of secondary beams
preparation for installing the roof
panels – placing the sealant strips
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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ELEMENTS SUBJECTED TO BENDING
Glass roof for refectory at the TU Dresden, 2006
TESTS 1:1• position of loads – joints,
eccentricity 120mm
• load-bearing capacity
• residual capacity of beams
• cyclic load, long term load
• deflection
Maximum breaking load 4,5
times higher than design load
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Glass roof for university of Glasgow, 2002
• triangular shape of glass roof
• maximum span 15,5m = 4x 3,9m,beams distance of 1,5m
• tempered glass 2x 19mm, friction grip
connection
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Glass roof for dry dock – Bristol, 2005
• historic passenger liner built from iron special dry dock to protect ship hull
• plates 2x 10mm heat-strengthened glass with size 4,35 x 1,5m – at waterline
• area 1000m2, 50mm of water weighing about 50 t – illusion of the dock
• the ship expand, contract and bend sideways in response to shifts in
temperature junction between the waterline plate and the ship had to
accommodate movements flexible collar
Practical examples
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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• beams: 3x 10mm heat-strengthened laminated glass, supportedon steel beams of trapezoidal cross-section, propped by struts
• accidental design case – dropping of a hammer from 15m, personfailing from deck, occasional foot traffic on the glass for cleaning
Practical examples
Glass roof for dry dock – Bristol, 2005
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Experimental research
LTB
Experiments
LTB of 3m laminated beam Belis, 2005 (UGent)
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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LTB
Experiments
LTB of 3m laminated beam Belis, 2005 (UGent)
Experimental researchObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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LTB
Experiments
LTB of 3m laminated beam Belis, 2005 (UGent)
Experimental researchObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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LTB
Experiments
LTB of 3m laminated beam
Belis, 2005 (UGent)
Experimental researchObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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LTB
Experiments
LTB of 3m laminated beam
Belis, 2005 (UGent)
Experimental researchObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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GLASS BEAMS
• horizontal elements• simply supported, cantilevering
• maximum length: float glass - 6,0 m
laminated glass - 4,5 m
tempered glass - 3,9 m
GLASS FINS • vertical or sloping beams used to support facades, wind load
• simple supported or fully cantilevering• longer than L 8m are usually top-hang shorter are bottom supported
DESIGN METHOD
• design according to the elastic stability
• finite elements methods
• tests 1:1
• how the overall structure will behave
• how the structure will behave after one or more glass elements
have failed
• safety of people at failure - injury by falling glass
Elements subjected to bendingObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Ultimate limit state
simplified check of lateral and torsional stability based on
M max maximum unfactored destabilising bending moment
E Young's modulus of elasticity
t thickness of the glass pane
υ Poisson's ratio
• it is possible to use for checking of buckling for glass fin with free
edges (without intermediate buckling restraint)
16
Et M M
3
max Ed
Elements subjected to bendingObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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LINEAR THEORY OF ELASTICITY
• perfect elastic beam without any imperfections with rectangular cross-section is subjected to an increasing load – bending moment M
• instability (combination of lateral deflection and twisting) occurs
suddenly when a critical load is reached M = MCR, where critical
torsional buckling moment is
• for rectangular cross-section including warping torsion
t y CR GI EI L
M
t 2
w 2
t y CR GI L
EI
1GI EI LM
Lateral torsional buckling
simplified formula without
warping torsion - conservative
simply supported beam loaded
by constant bending moment
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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LINEAR THEORY OF ELASTICITY
• perfect elastic beam without any imperfections with rectangular cross-section is subjected to an increasing load – bending moment M
• instability (combination of lateral deflection and twisting) occurs
suddenly when a critical load is reached M = MCR, where critical
torsional buckling moment is
• for rectangular cross-section including warping torsion
t y CR GI EI L
M
t 2
w 2
t y CR GI L
EI
1GI EI LM
Lateral torsional buckling
bending stiffness
simplified formula without
warping torsion - conservative
simply supported beam loaded
by constant bending moment
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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LINEAR THEORY OF ELASTICITY
• perfect elastic beam without any imperfections with rectangular cross-section is subjected to an increasing load – bending moment M
• instability (combination of lateral deflection and twisting) occurs
suddenly when a critical load is reached M = MCR, where critical
torsional buckling moment is
• for rectangular cross-section including warping torsion
t y CR GI EI L
M
t 2
w 2
t y CR GI L
EI
1GI EI LM
Lateral torsional buckling
torsional stiffness simplified formula withoutwarping torsion - conservative
simply supported beam loaded
by constant bending moment
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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LINEAR THEORY OF ELASTICITY
• perfect elastic beam without any imperfections with rectangular cross-section is subjected to an increasing load – bending moment M
• instability (combination of lateral deflection and twisting) occurs
suddenly when a critical load is reached M = MCR, where critical
torsional buckling moment is
• for rectangular cross-section including warping torsion
t y CR GI EI L
M
t 2
w 2
t y CR GI L
EI
1GI EI LM
Lateral torsional buckling
simplified formula without
warping torsion - conservative
simply supported beam loaded
by constant bending moment
critical length
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Critical torsional buckling moment depends on:
• different moment distribution over the beam
• boundary conditions
• distance between the centre of gravity and the point where the
load is applied
Lateral torsional buckling
Influence of following aspects on behaviour of glass
beams must be taken into account:
• glass thickness
• initial deformation – float x tempered glass
• laminated glass: shear modulus of PVB foil temperature
• load duration• damage of glass surface
• tensile strength of glass
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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RESEARCH BASED ON EXPERIMENTAL TESTS
EPFL, Lausanne, Switzerland
• simple supported beam, concentrated load at mid-span
• stress distribution is nonlinear over the beam height
• lateral torsional buckling resistance is not limited by the critical
torsional buckling moment
• tensile strength of glass is determinant for the buckling resistance
• influence of elastic interlayer (PVB foil) on the buckling strength –
temperature, load duration, thickness of the glass as well as
thickness of the interlayer
Lateral torsional bucklingObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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A) Monolithic glass – Analytical model
Critical LTB
Moment
Lateral torsional buckling
a
z
t
a z
CR z C
EI
LGI z C
L
EI C M 22
2
2
22
2
1
• C i , z a …take into account different boundary conditions, different bending
moment, distance between the centre of gravity and the load point
• LTB formulas for steel are valid, e.g. EC3
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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B) Laminated glass – Analytical model
• No homogene, isotropic material
• Shear deformation due to lateral
bending & torsion
Belis, 2005 (UGent)Critical LTB
Moment
Lateral torsional buckling
a
eff z g
eff t
a
eff z g
CR z C I E
LGI z C
L
I E C M 22
2
2
22
2
1
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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B) Laminated glass – Analytical model
• No homogene, isotropic material
• Shear deformation due to lateral
bending & torsion
Belis, 2005 (UGent)Critical LTB
Moment
Lateral torsional buckling
a
eff z g
eff t
a
eff z g
CR z C I E
LGI z C
L
I E C M 22
2
2
22
2
1
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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• it is possible to use same formula for MCR
• lateral bending stiffness EIz and the torsional stiffness GIt are replaced by an
equivalent stiffness (EgIz)eff a (GIt)eff (determined by sandwich theory )
Effective bending stiffness (EgIz)eff
B) Laminated glass – Analytical model
Lateral torsional buckling
2
2
1
1 s g eff z g
I E I E ht t
t t t
t t I
g g
g g
int
g g
s
21
21
2
21
24
Luible
Wölfel
slower , z g eff z g B I E I E
2
2121
2
int g g
int g
int
g
g
s
t t Wt
L
t t
G
E
E B
α, β – same formulas as for compression member
Objectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Effective torsional stiffness (GIt)eff
y
x
z
t1 t
2tPVB
h
PVB
Glas
Glas
MT B
tg1 tint tg2
B) Laminated glass – Analytical model
Luible
Scarpino
compt glasst glasst eff t
GI GI GI GI 21
2
21h
htanh
GI GI scompt
21
21
g g int
g g int
t t t
t t
G
G
f GI GI t eff t
22
2223
6
3646
W G
Gt t t
t t t t W G
Gt t
f
g
int int g g
g int g int
g
int int g
Lateral torsional bucklingObjectives
Introduction
Experimental
research
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Interlayer shear stiffness - Gint
Lateral torsional buckling
• Influence of the shear modulus GPVB on the critical lateral torsional bucklingload Mcr,LT
• The curves ratio Mcr,LT / Mcr,LT, without PVB
Objectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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• calculation of structure with initial imperfections
• too complicated unsuitable for design of beams
C) Non-linear buckling analysis – second order calculation
Lateral torsional buckling
B) Laminated glass – Analytical model
• Stress problem is not solved analytically
Objectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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D) Laminated glass – Numerical model
Luible, 2004 (EPFL)
x
yz
Axis ofsymmetry
glass
u
vw
v 0
fork
support
φx
φy
φz
Bonding condition:
u=0, φy=φz=0
F/2
Lateral torsional bucklingObjectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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D) Laminated glass – Numerical model
Luible, 2004 (EPFL)
x
yz
Axis ofsymmetry
glass
u
vw
v 0
fork
support
φx
φy
φz
Bonding condition:
u=0, φy=φz=0
F/2
tPVB= 0
= 0t1
PVB (solid element)elastic or viscoelastic
Equal nodes glass(shell element)
with offset t/2
Lateral torsional bucklingObjectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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D) Laminated glass – Numerical model
Luible, 2004 (EPFL)
x
yz
Axis ofsymmetry
glass
u
vw
v 0
fork
support
φx
φy
φz
Bonding condition:
u=0, φy=φz=0
F/2
tPVB= 0
= 0t1
PVB (solid element)elastic or viscoelastic
Equal nodes glass(shell element)
with offset t/2
tPVB = 0
11
740
44My
5
9
coupling
PVB
glassBeam element
Lateral torsional bucklingObjectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Only existing code:
Australian Standard AS 1288: Glass in Buildings – selection andinstallation
Appendix C: Buckling of glass fins
Simple approach
Better design approaches:
• Non linear numerical model inlculding all imperfections
• Buckling curves
Design methods
71 ,
M M cr Ed
Objectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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determination of the lateral and torsional buckling
resistance
1) an appropriate FE model: tensile stress on glass surfaces can becompared to tensile strength - complicated
2) buckling curves
• slenderness ratio depends on tensile strength of the glass
where
σ p,t - tensile strength of glass,
σ CR - critical lateral torsional buckling stress,
M cr - elastic critical moment
hM
I 2
CR
y t , p
CR
t , p
Design methodsObjectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Design – buckling curve
• Slenderness
• Reduction factor LTB
• Bending strength taking into
account LTB
• Verification
D
0.0
0.2
0.4
0.6
0.8
1.0
1.2
0.0 0.5 1.0 1.5 2.0 2.5
D coefficient d’élancement
au déversement
,
,
p t D
cr D
,
y D
p t
slenderness
Design methods
h M
I
CR
yt , p
CR
t , p
LT
2
yt , p LT
y
t , p LT Rd W I
M 2
LT LT f
Ed Rd M M
LT
LT
LT
LT
Objectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Design – buckling curve
• Slenderness
• Reduction factor LTB
• Bending strength taking into
account LTB
• Verification
D
0.0
0.2
0.4
0.6
0.8
1.0
1.2
0.0 0.5 1.0 1.5 2.0 2.5
D coefficient d’élancement
au déversement
,
,
p t D
cr D
,
y D
p t
slenderness
Design methods
h M
I
CR
yt , p
CR
t , p
LT
2
yt , p LT
y
t , p LT Rd W I
M 2
LT LT f
Ed Rd M M
LT
LT
LT
LT
Objectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Design – buckling curve
• Slenderness
• Reduction factor LTB
• Bending strength taking into
account LTB
• Verification
D
0.0
0.2
0.4
0.6
0.8
1.0
1.2
0.0 0.5 1.0 1.5 2.0 2.5
D coefficient d’élancement
au déversement
,
,
p t D
cr D
,
y D
p t
slenderness
LTB buckling curves need to
be established for glass
Design methods
h M
I
CR
yt , p
CR
t , p
LT
2
yt , p LT
y
t , p LT Rd W I
M 2
LT LT f
Ed Rd M M
LT
LT
LT
LT
Objectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Design – buckling curve
Design methods
slenderness LT
• for different types of loading, glass geometries, shear modulus of PVB
interlayer and initial deformations it is possible derived different buckling
curves reduction factor
• buckling curve (c) from Eurocode may be used as a conservative approach
Objectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Australian standard AS 1288 - 1994: apendix H
1. Beams with intermediate buckling restraints
where M CR critical elastic buckling moment
g 1 constant from table
Lay distance between effectively rigid buckling restraints
(EI)y effective rigidity for bending about the minor axis
GJ effective torsional rigidity
J torsional moment of inertia
for rectangular cross-section
d, b depth and breadth of the beam
501 , yay
CR GJ EI L g
M
d
b ,
db J 6301
3
3
Design methodsObjectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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intermediate buckling
restraintside view of beam
top view of beam
M
z
Lay
M
z
y
y
x
x
free restraint condition fixed restraint condition
1,0 3,1 6,3
0,5 4,1 8,20,0 5,5 11,1
-0,5 7,3 14,0
-1,0 8,0 14,0
Coefficient g1 Moment parameter
β = M1 / M2
Design methodsObjectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Australian standard AS 1288 - 1994: apendix H
2. Beams without intermediate buckling restraint
where M CR critical elastic buckling moment
g 2 , g 3 constants from table
Lay distance between effectively rigid buckling restrains
(span of beam)
(EI)y effective rigidity for bending about the minor axis
GJ effective torsional rigidity
y h height above centroid of the point of load application
5 ,0 y ay h35 ,0 y ay
2 CR GJ EI L / y g 1GJ EI L
g M
Design methodsObjectives
Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Type of loading Bending moment MCondition of endrestraint againstrotation about y-y
Coefficient
g2
g3
free
fixed
3,6
6,1
1,4
1,8
free
fixed
4,1
5,4
4,9
5,2
free
fixed
4,2
6,7
1,7
2,6
free
fixed
5,3
6,5
4,5
5,3
free
fixed
3,3
-
1,3
-
Lay 8
wL2 ay
Lay 12
wL2 ay
4
FLay
8
FLay
8
FLay
Lay
F
Lay
F
Lay
F/2 F/2
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Introduction
Experimentalresearch
Elements
subjected to
bending
Lateral torsional
buckling
Design methods
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Australian standard AS 1288 - 1994: apendix H
3. Continuously restrained beams on tension side
where M CR critical elastic buckling moment
Lay distance between points of effective rigid rotational
restraints
(EI)y effective rigidity for bending about the minor axis
GJ effective torsional rigidity
d depth of beamy h location above the neutral axis of the loading point,
positive or negative values
y 0 distance of the restraints from neutral axis
h0
2 0
2
y
2 a
CR y y 2
GJ y 4
d EI L
M
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Lateral torsional
buckling
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Serviceability limit state
• deflection, vibration
• simple rule for natural frequency
where d midspan deflection of beam or tip deflection of cantilever [mm]f first natural frequency [Hz] - foot traffic and wind
Float glass – low tension stress levels usually deflection is not
problem
Laminated or tempered glass – higher stress levels important
check of deflection
Hz 5 d
16 f
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Experimentalresearch
Elements
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Lateral torsional
buckling
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References
Educational pack of COSTActin TU0905 „Structural Glass - Novel design methods and next generation
products“
HALDIMANN, Matthias; LUIBLE, Andreas; OVEREND, Mauro.Structural Use of Glass. Structural Engineering Documents 10 , IABSE, Zürich:2008. ISBN 978-3-85748-
119-2
THE INSTITUTION OF STRUCTURAL ENGINEERS
Structural use of glass in buildings, London: The institution of Structural Engineers, 1999.
KASPER, Ruth.
Tragverhalten von Glasträgern, RWTH Aachen, Aachen: Shaker Verlag, 2005.
Australian Standard AS 1288.
Glass in Buildings – Selection and installation, Appendix C: Basis for determination of fin design to prevent
buckling, 2006.
AMADIO, Claudio; BEDON, Chiara.
Buckling of laminated glass elements in out-of-plane bending, Engineering Structures 32 (2010), 3780–
3788.
BELIS, Jan; MOCIBOB, Danijel; LUIBLE, Andreas; VANDEBROEK, Marc.
On the size and shape of initial out-of-plane curvatures in structural glass components, Construction and
Building Materials 25 (2011), 2700–2712.
LUIBLE, A.
Stabilität von Tragelementen aus Glas. Dissertation EPFL thèse 3014. Lausanne: 2004.
LINDNER, J.; HOLBERNDT, T.
Zum Nachweis von stabilitätsgefährdeten Glasträgern unter Biegebeanspruchung. Stahlbau 75(6) (2006),
488-498.
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Thank you
for your kind attention
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