Advances in compositestructures design and simulationTRAINING MODULES
for Researchers
Volume 3
2015
National Aerospace University
“KhAI”
Advances in compositestructures design and simulationTRAINING MODULES
for Researchers
Volume 3
2015
National Aerospace University
“KhAI”
Advances in compositestructures design and simulationTRAINING MODULES
for Researchers
Volume 3
2015
National Aerospace University
“KhAI”
Advances in composite structuresdesign and simulation
Volume 3
TRAINING MODULES
for Researchers
Prepared in the frame of the FP7 KhAI-ERA project activities
2015
Institute of Aerospace Engineering - Brno University of Technology “IAE-BUT”
Advances in composite structuresdesign and simulation
Volume 3
TRAINING MODULES
for Researchers
Prepared in the frame of the FP7 KhAI-ERA project activities
2015
Institute of Aerospace Engineering - Brno University of Technology “IAE-BUT”
Advances in composite structuresdesign and simulation
Volume 3
TRAINING MODULES
for Researchers
Prepared in the frame of the FP7 KhAI-ERA project activities
2015
Institute of Aerospace Engineering - Brno University of Technology “IAE-BUT”
Published by the National Aerospace University “KhAI” in 2015
Advances in composite structures design and simulation
This training modules collection was jointly prepared by the National Aerospace University “KhAI” andInstitute of Aerospace Engineering, Brno University of Technology (IAE-BUT) in the frame of FP7 KhAI-ERAproject training development activities. It is intended for researchers interested in composite structures.Included to this issue training modules are presentations of buckling and post-buckling simulationsincluding post-processing and examples; nonlinear explicit FE analysis application for impact problemssimulation, and finite element modelling and analysis using Python.
Reproduction is authorised provided the source is acknowledged. No use of this publication may be madefor resale or for any other commercial purpose.
Available on-line at http://khai-era.khai.edu/en/site/training-modules.html
For enquiries, inputs and feedback on the use of this document please contact:
International S&T Projects Office
National Aerospace University “KhAI”
17Chkalova str., Kharkov, 61070, Ukraine
Phone: +38 (057) 788 40 60
Fax: +38 (057) 719 04 73
e-mail: [email protected]
LEGAL NOTICE
Neither the European Commission nor any person acting on behalf of the Commission is responsible for theuse, which might be made, of the following information.
The views expressed in this report are those of the authors and do not necessarily reflect those of theEuropean Commission.
© KhAI-ERA Consortium, 2015
Foreword
This material arose by the KhAI-ERA project as a result of knowledge exchange by researchers of Institute ofAerospace Engineering - Brno University of Technology (hereinafter IAE-BUT) to researchers of NationalAerospace University (hereinafter KhAI).
The publication shows the collection of training modules where aspects and examples of advanced finiteelement analysis methods application for composite aeronautic structures are presented.
Assoc. prof. Jaroslav JuračkaInstitute of Aerospace Engineering - Brno University of Technology
Authors
Assoc. prof. Jaroslav JuračkaIAE-BUT
Assoc. prof. Juracka is Director of the IAE-BUT. His research is focussed onaircraft design, structural analysis, composite structures, and aircrafttesting. He has considerable experience of applied industrial projectsincluding – CEDESA (coordinator, FP7, 2010-2014), Development of VUT 001Marabu aircraft for UAV applications (2006-2009), Development of EV-55airplane in cooperation with EVEKTOR (2005-2010), Development ofVUT100 Cobra aircraft (2002-2006), Cost Effective Small Aircraft - CESAR(FP6 Project, 2006-2009)
Dr. Michal MališIAE-BUT
Dr. Michal Mališ is a researcher of NETME Centre. He participates innational projects named “Advanced Aerostructures Research Centre” and“Crash”. His research is focused on crashworthiness of light aircrafts andfinite element method simulations of statically and dynamically loaded thin-walled structures, mainly made out of composite materials. He wasresponsible for stress analyses and design of supporting structures fromcomposite materials of VUT 001 Marabu, VUT 061 Turbo and VUT 081KONDOR aircrafts. He is author of the COMPOST software - COMpositePOST processor for finite element solvers.
M.Sc. Volodymyr SymonovIAE-BUT
Volodymyr Symonov is a researcher of NETME Centre. He participates in thenational project named “Advanced Aerostructures Research Centre”. Hisresearch is focused mainly on aircraft structures made of compositematerials. Particularly his scientific interests are connected with estimationof aircraft primary structures life, metal-composite and composite-composite joints design, stress analysis, tests and finite element simulationsof statically and dynamically loaded thin-walled structures and joints. Heparticipated in stress analysis and finite element simulations of L410 NGaircraft within MOSTA project and also participated in FP7 CEDESA project.
Authors
Assoc. prof. Jaroslav JuračkaIAE-BUT
Assoc. prof. Juracka is Director of the IAE-BUT. His research is focussed onaircraft design, structural analysis, composite structures, and aircrafttesting. He has considerable experience of applied industrial projectsincluding – CEDESA (coordinator, FP7, 2010-2014), Development of VUT 001Marabu aircraft for UAV applications (2006-2009), Development of EV-55airplane in cooperation with EVEKTOR (2005-2010), Development ofVUT100 Cobra aircraft (2002-2006), Cost Effective Small Aircraft - CESAR(FP6 Project, 2006-2009)
Dr. Michal MališIAE-BUT
Dr. Michal Mališ is a researcher of NETME Centre. He participates innational projects named “Advanced Aerostructures Research Centre” and“Crash”. His research is focused on crashworthiness of light aircrafts andfinite element method simulations of statically and dynamically loaded thin-walled structures, mainly made out of composite materials. He wasresponsible for stress analyses and design of supporting structures fromcomposite materials of VUT 001 Marabu, VUT 061 Turbo and VUT 081KONDOR aircrafts. He is author of the COMPOST software - COMpositePOST processor for finite element solvers.
M.Sc. Volodymyr SymonovIAE-BUT
Volodymyr Symonov is a researcher of NETME Centre. He participates in thenational project named “Advanced Aerostructures Research Centre”. Hisresearch is focused mainly on aircraft structures made of compositematerials. Particularly his scientific interests are connected with estimationof aircraft primary structures life, metal-composite and composite-composite joints design, stress analysis, tests and finite element simulationsof statically and dynamically loaded thin-walled structures and joints. Heparticipated in stress analysis and finite element simulations of L410 NGaircraft within MOSTA project and also participated in FP7 CEDESA project.
Authors
Assoc. prof. Jaroslav JuračkaIAE-BUT
Assoc. prof. Juracka is Director of the IAE-BUT. His research is focussed onaircraft design, structural analysis, composite structures, and aircrafttesting. He has considerable experience of applied industrial projectsincluding – CEDESA (coordinator, FP7, 2010-2014), Development of VUT 001Marabu aircraft for UAV applications (2006-2009), Development of EV-55airplane in cooperation with EVEKTOR (2005-2010), Development ofVUT100 Cobra aircraft (2002-2006), Cost Effective Small Aircraft - CESAR(FP6 Project, 2006-2009)
Dr. Michal MališIAE-BUT
Dr. Michal Mališ is a researcher of NETME Centre. He participates innational projects named “Advanced Aerostructures Research Centre” and“Crash”. His research is focused on crashworthiness of light aircrafts andfinite element method simulations of statically and dynamically loaded thin-walled structures, mainly made out of composite materials. He wasresponsible for stress analyses and design of supporting structures fromcomposite materials of VUT 001 Marabu, VUT 061 Turbo and VUT 081KONDOR aircrafts. He is author of the COMPOST software - COMpositePOST processor for finite element solvers.
M.Sc. Volodymyr SymonovIAE-BUT
Volodymyr Symonov is a researcher of NETME Centre. He participates in thenational project named “Advanced Aerostructures Research Centre”. Hisresearch is focused mainly on aircraft structures made of compositematerials. Particularly his scientific interests are connected with estimationof aircraft primary structures life, metal-composite and composite-composite joints design, stress analysis, tests and finite element simulationsof statically and dynamically loaded thin-walled structures and joints. Heparticipated in stress analysis and finite element simulations of L410 NGaircraft within MOSTA project and also participated in FP7 CEDESA project.
M.Sc. Pavel SchořIAE-BUT
Pavel Schoř is a PhD. student at Institute of Aerospace Engineering.His PhD. research is mainly focused on numerical solving of staticaero-elastic problems, but he is also involved in structural problems.He is co-designer of composite landing gear spring for VUT 061 Turboairplane and co-author of the COMPOST software.
Content
Module 1 Post-buckling simulations and post-processing including examples 10Dr. Michal Mališ, IAE-BUT
Buckling Problem 13
Outline 14
Example problem. Thin-walled unstiffened cylinder 14
Parameters affecting buckling load analysis 16
Parameters affecting FEM analysis results 17
Analytical solution 17
Influence of Plies orientation 20
Comparison of FEA and analytical solution results 20
Geometrical imperfection Analysis 23
Module 2 Nonlinear explicit FE analysis application for impact problemssimulation 30
M.Sc. Volodymyr Symonov, IAE-BUT
Explicit and Implicit Methods 33
Bird Strike Simulations 35
MSC Nastran/Dytran Material Models 37
Modelling of Interlaminar Delamination 38
Contact Modelling 38
Module 3 FE modelling and analysis using Python 40
M.Sc. Pavel Schoř, IAE-BUT
Example problem 44
Introduction to Abaqus scripting 50
Example - flat plate with mesh 50
Material imperfections 51
Module for creating imperfect plates 53
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 11
Training Module 1
Post-Buckling Simulations and Post-ProcessingIncluding Examples
Dr. Michal Mališ
IAE-BUT
2015
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 13
Introduction
Thin-walled structures are widely used in aerospace vehicles. A simple representative of such a structurecan be a thin-walled cylinder. The most critical failure mode for this type of structures is buckling.Therefore, it is very important to correctly define the buckling load of the structure. The results of FEbuckling simulations depend on many aspects including material model used and special numericalparameters such as time step, etc. Therefore, it is very important to select appropriate parameters in orderto obtain correct simulation results including correct post-buckling behavior of the structure.
This module describes how to adjust FE model of an axially compressed thin-walled unstiffened cylinder inorder to meet correlation with test results, and analytical solution.
One of the aspects influencing the correlation between the simulation and test results is imperfectionsoccurred in a real structure which weaken the structure leading to lower buckling load. Several approachesfor imitating imperfections in FE models are described and compared in the module.
Module components
Buckling of thin-walled unstiffened cylinders
FEA vs. analytical solution results
Geometrical imperfections
Target audience
doctoral and master students, researchers
Advances in composite structures design and simulation
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Reference [6]
Advances in composite structures design and simulation
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Reference [6]
Advances in composite structures design and simulation
14 Prepared in the frame of the FP7 KhAI-ERA project
Reference [6]
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 15
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 15
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 15
Advances in composite structures design and simulation
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Advances in composite structures design and simulation
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Advances in composite structures design and simulation
16 Prepared in the frame of the FP7 KhAI-ERA project
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 17
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 17
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 17
Advances in composite structures design and simulation
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Advances in composite structures design and simulation
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Advances in composite structures design and simulation
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Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 19
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 19
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 19
Advances in composite structures design and simulation
20 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
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Advances in composite structures design and simulation
20 Prepared in the frame of the FP7 KhAI-ERA project
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 21
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 21
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 21
Advances in composite structures design and simulation
22 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
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Advances in composite structures design and simulation
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Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 23
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 23
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 23
Advances in composite structures design and simulation
24 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
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Advances in composite structures design and simulation
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Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 25
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 25
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 25
Advances in composite structures design and simulation
26 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
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Advances in composite structures design and simulation
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Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 27
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 27
Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 27
Advances in composite structures design and simulation
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Advances in composite structures design and simulation
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Advances in composite structures design and simulation
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Module 1 – Post-Buckling Simulations and Post-Processing Including Examples
Prepared in the frame of the FP7 KhAI-ERA project 29
References
1. Geier,B., Meyer-Piening, H., Zimmermann, R.: „On the influence of laminate stackingsequences of composite cylindrical shell subjected to axial compression”, Compositesstructures, 55, page 467-474, 2002.
2. Degenhardt R., Kling A., Rohwer K., Orifici A. C., Thomson R. S., “Design and Analysis ofStiffened Composite Panels Including Postbuckling and Collapse”, Computers and StructuresVol. 86 (2008), pp. 919-929
3. Hühne,C., Rolfes,R., Breitbach, E., Tessmer, J.: „Robust design of composite cylindrical shellsunder axial compression – Simulation and validation ”, Thin-Walled Structures, 46, page 947-962, 2008.
4. Kriegesmann, Benedikt:, „Probabilistic Design of thin-walled fiber composite structures”,Dissertation. Leibnitz Universität Hannover, 2012.
5. Steinmüler, Patrick:, „Investigation of axially loaded unstiffened CFRP cylindrical shellssubjected to single perturbation loads”, Master thesis, Private university of applied scienceGöttingen, 2008.
6. FP7 DESICOS project: [web-site]. URL: http://www.desicos.eu (reference date: 01.04.2015)
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 31
Training Module 2
Nonlinear Explicit FE Analysis Application forImpact Problems Simulation
M.Sc. Volodymyr Symonov
IAE-BUT
2015
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 33
Introduction
The impact analysis requires complex multidisciplinary approach. The best way to assess the impactresistibility of a structure is a real experiment which is very expensive. A good alternative to the experimentcan be FE simulations. Because impact is a dynamic transition process special FE methods should be usedfor its simulation called implicit and explicit analyses.
The current module describes the differences and application scope of explicit and implicit methods.
Bird strike FE analysis represents the explicit method application for impact problem simulation. The mainaspects of bird strike analysis are described in the module.
Module components
Explicit vs. Implicit FEA methods
Bird Strike Simulation Major Aspects
Target audience
doctoral and master students, researchers
Advances in composite structures design and simulation
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Advances in composite structures design and simulation
34 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
34 Prepared in the frame of the FP7 KhAI-ERA project
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 35
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 35
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 35
Advances in composite structures design and simulation
36 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
36 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
36 Prepared in the frame of the FP7 KhAI-ERA project
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 37
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 37
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 37
Advances in composite structures design and simulation
38 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
38 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
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Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 39
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 39
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 39
Advances in composite structures design and simulation
40 Prepared in the frame of the FP7 KhAI-ERA project
References
7. MSC Nastran 2013 Explicit Nonlinear (SOL 700) User’s Guide.
8. Tho, C.H., Smith, M.R. : „Accurate bird strike simulation methodology for ba609 tiltrotor”,Journal of the American Helicopter Society, 56(1), pp.12007, 2011.
9. Heimbs, S.: “Computational methods for bird strike simulations: A review”, Computers andStructures, 89, page 2093-2112, 2011.
10. Lavoie, M.A., Gakwaya, A., Ensan, M.N., Zimcik, D.G., Nandlall, D.: “Bird’s substitute testsresults and evaluation of available numerical methods”, International Journal of ImpactEngineering, 36, page 1276–1287, 2009.
11. Hedayati, R., Sadighi, M., Mohammadi-Aghdam, M.: “On the difference of pressure readingsfrom the numerical, experimental and theoretical results in different bird strike studies”,Aerospace Science and Technology, 32, page 260–266, 2014.
12. Heimbs, S., Bergmann, T., Schueler, D., Toso-Pentecôte, N.: “High velocity impact onpreloaded composite plates”, Composite Structures, 111, page 158-168, 2014.
13. Abdullah, E., Ferrero, J.-F., Barrau, J.-J., Mouillet, J.-B.: ”Development of a new finite elementfor composite delamination analysis”, Composites Science and Technology, 67, page 2208–2218, 2007.
14. Heimbs, S.: “Bird Strike Simulations on Composite Aircraft Structures”, 23rd SIMULIACustomer Conference, May 17-19, 2011, Barcelona, Spain.
Module 2 – Nonlinear Explicit FE Analysis Application for Impact Problems Simulation
Prepared in the frame of the FP7 KhAI-ERA project 41
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 43
Training Module 3
FE Modelling and Analysis Using Python
M.Sc. Pavel Schoř
IAE-BUT
2015
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 45
Introduction
Many specific structural analysis problems require flexible and complex approach which cannot beachieved with conventional application of FE modelling and analysis. These aspects can be covered withhelp of joining FE modelling and programming capabilities. One of the most worldwide spreadprogramming languages for engineers is Python.
This module describes how to apply Python for FE modelling of a specific problem in Abaqus based on anexample problem which is connected to imperfect composite parts.
Module components
Application of Python for FE modelling
Example problem. Simulations of imperfect composite parts
Target audience
doctoral and master students, researchers
Advances in composite structures design and simulation
46 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
46 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
46 Prepared in the frame of the FP7 KhAI-ERA project
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 47
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 47
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 47
Advances in composite structures design and simulation
48 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
48 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
48 Prepared in the frame of the FP7 KhAI-ERA project
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 49
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 49
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 49
Advances in composite structures design and simulation
50 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
50 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
50 Prepared in the frame of the FP7 KhAI-ERA project
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 51
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 51
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 51
Advances in composite structures design and simulation
52 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
52 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
52 Prepared in the frame of the FP7 KhAI-ERA project
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 53
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 53
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 53
Advances in composite structures design and simulation
54 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
54 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
54 Prepared in the frame of the FP7 KhAI-ERA project
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 55
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 55
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 55
Advances in composite structures design and simulation
56 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
56 Prepared in the frame of the FP7 KhAI-ERA project
Advances in composite structures design and simulation
56 Prepared in the frame of the FP7 KhAI-ERA project
Module 3 – FE Modelling and Analysis Using Python
Prepared in the frame of the FP7 KhAI-ERA project 57
References
1. Abaqus user manual.
2. Abaqus scripting manual.
3. Python for aerospace engineers.
4. Example scripts.
5. BMP2TI Utility.
Prepared under the aegis of KhAI-ERA projectfunded by the European Commission’s Directorate-Generalfor Research & Innovations under the FP7 CapacitiesSpecific Programme on International CooperationGrant Agreement no 294311National Aerospace University
“KhAI”17 Chkalova str., Kharkiv
61070 Ukrainewww.khai.edu
Prepared under the aegis of KhAI-ERA projectfunded by the European Commission’s Directorate-Generalfor Research & Innovations under the FP7 CapacitiesSpecific Programme on International CooperationGrant Agreement no 294311National Aerospace University
“KhAI”17 Chkalova str., Kharkiv
61070 Ukrainewww.khai.edu
Prepared under the aegis of KhAI-ERA projectfunded by the European Commission’s Directorate-Generalfor Research & Innovations under the FP7 CapacitiesSpecific Programme on International CooperationGrant Agreement no 294311National Aerospace University
“KhAI”17 Chkalova str., Kharkiv
61070 Ukrainewww.khai.edu