COCOMAT
Publications of COCOMAT results
| No. |
Authors
|
Titles
|
Name of Conference /
Magazine |
Pages
|
Date / Place
|
Downloads
|
| 2008 ( partly planned) | ||||||
| 64 | Orifici, A.C., Thomson, R.S., Degenhardt, R., Bisagni, C., Bayandor, J. | A finite element methodology for analysing degradation and collapse in postbuckling composite aerospace structures | Journal of Composite Materials | paper submitted | ||
| 63 | Orifici, A.C., Ortiz de Zarate Alberdi, I., Thomson, R.S., Bayandor, J. | Compression and postbuckling damage growth and collapse analysis of flat composite stiffened panels | Composite Science and Technology | in press | ||
| 62 | Orifici, A.C., Thomson, R.S., Degenhardt, R. | The design of postbuckling composite aerospace structures accounting for damage initiation and growth | International Council of the Aeronautical Sciences 2008 Congress | 4-19 September, Anchorage, USA | ||
| 61 | Lee. M.C.W., Thomson, R.S., Degenhardt, R., Kelly, D.W. | Imperfection investigation of composite stiffened fuselage panels for postbuckling analyses | 5th International Conference on Thin-Walled Structures | 18-20 June, Brisbane, Australia | ||
| 59/60 | Orifici, A.C., Kotler, A., Abramovich, H., Herszberg, I., Weller, T.. | Failure in CFRP L-stiffened panel sections under postbuckling loads | 48th Israel Annual Conference on Aerospace Sciences | 27-28 February, Tel Aviv/Haifa, Israel | ||
| 2007 ( partly planned) | ||||||
| 58 | Orifici, A.C., Thomson, R.S., Degenhardt, R., Bisagni, C., Bayandor, J. | Development of a degradation model for the propagation of delaminations in composite structures | Computers, Materials & Continua | paper submitted | ||
| 57 | Lee, M.C.W., Payne, R., Kelly, D.W., Thomson, R.S. | Determination of robustness for a stiffened composite structure using stochastic analysis | Composite Structures, Vol. 86 |
pp. 78-84 | ||
| 56 | Orifici, A.C., Shah, S.A., Herszberg, I., Kotler, A., Weller, T. | Failure analysis in postbuckled composite T-sections | Composite Structures, Vol. 86 |
pp. 146-153 | ||
| 55 | Orifici, A.C., Ortiz de Zarate Alberdi, I., Thomson, R.S., Bayandor, J. | Damage growth and collapse analysis of composite blade-stiffened structures | 14th International Conference on Composite Structures | 19-21 November, Melbourne, Australia | ||
| 54 | Orifici, A.C., Thomson, R.S., Herszberg, I., Weller, T., Degenhardt, R., Bayandor, J. | An analysis methodology for failure in postbuckling skin-stiffener interfaces | Composite Structures, Vol. 86 |
pp. 186-193 | ||
| 53 | Degenhardt, R., Kling, A., Rohwer, K., Orifici, A.C., Thomson, R.S. | Design and analysis of stiffened composite panels including post-buckling and collapse | Computers and Structures, Vol. 86 |
pp. 919-929 | ||
| 52 | Orifici, A.C., Thomson, R.S, Degenhardt, R., Bayandor, J. | Development of a finite element methodology for the collapse analysis of composite aerospace structures | ECCOMAS Thematic Conference on Mechanical Response of Composites | 12-14 September, Porto, Portugal | ||
| 51 | Lee, M., Kelly, D., Orifici, A.C., Thomson, R.S. | Postbuckling mode shapes of composite stiffened fuselage panels incorporating stochastic variables | 1st CEAS European Air and Space Conference | 10-13 September, Berlin, Germany | ||
| 50 | Scott, M.L., Thomson, R.S., Gunnion, A.J., Orifici, A.C. | Simulation of defects and damage: Towards a virtual testing laboratory for composite aerospace structures | 1st CFK Valley Stade Convention | 13-14 June, Stade, Germany | ||
| 49 | Balzani, C., Wagner, W. | An Interface Element for the Simulation of Delamination in Uni-Directional Fiber-Reinforced Composite Laminates | Engineering Fracture Mechanics (2007) (in press) | |||
| 48 | Balzani, C., Wagner, W. | Simulation of skin-stiffener debonding in stiffened curved carbon/epoxy panels | 78th GAMM Annual Meeting | 16-20 July, Zurich, Switzerland | ||
| 47 | Elder, D., Thomson, R. | Probabilistic assessment of a stiffened carbon fibre composite panel operating in its postbuckled region | 6th European LS-DYNA Users Conference | 29-30 May, Gothenburg, Sweden | ||
| 46 | Rohwer K., Degenhardt R. | Simulating Postbuckling Behaviour and Collapse of Stiffened CFRP Panels | Proceedings of the NAFEMS World Congress 2007 | 22-25 May, Vancouver, Canada | ||
| 45 | Abramovich, H., Bisagni, C., Cordisco, P. | Post-buckling test simulation of a stiffened composite panel | Proceedings of the 48th AIAA Conference on Structures, Structural Dynamics and Materials | 23-26 April, Waikiki, Hawaii, USA | ||
| 44 | Degenhardt R., Tessmer J. | Improved Design Scenario for Composite Airframe Structures | Proceedings of the 48th AIAA Conference on Structures, Structural Dynamics and Materials | 23-26 April, Waikiki, Hawaii, USA | ||
| 43 | Orifici, AC, Thomson, R, Degenhardt, R, Kling, A, Rohwer, K, & Bayandor, J | Degradation investigation in a postbuckling composite stiffened panel | Composite Structures, Vol. 82, No. 2 |
pp. 217-224 | ||
| 42 | Orifici A. C., Thomson R. S., Degenhardt R., Bisagni C., Bayandor J. | Development of a finite element methodology for the propagation of delaminations in composite structures | Mechanics of Composite Materials, Vol. 43, No. 1 | pp. 9-28 | ||
| 41 | Wagner, W., Balzani, C. | Finite Element Simulation of Skin-Stiffener Debonding in curved panels of fiber-reinforced composite laminates | Proceedings of the 12th Australian International Aerospace Congress | pp. 1-12, ISBN 978-0-9803215-0-0 |
19-22 March, Melbourne, Australia | |
| 40 | Doreille M., Merazzi S., Degenhardt R., Kling A. | B2000++ A fast Analysis Tool for Stability Calculations of Composite Structures | Proceedings of the 12th Australian International Aerospace Congress | 19-22 March, Melbourne, Australia | ||
| 39 | Orifici A. C., Herszberg I., Thomson R. S., Weller T., Kotler A., Bayandor J. | Failure in stringer interfaces in postbuckled composite stiffened panels | Proceedings of the 12th Australian International Aerospace Congress | 19-22 March, Melbourne, Australia | ||
| 38 | Herszberg I., Kotler A., Orifici A. C., Abramovich H., Weller T. | Failure modes in loaded carbon/epoxy composite T-sections | Proceedings of the 12th Australian International Aerospace Congress | 19-22 March, Melbourne, Australia | ||
| 37 | Orifici A. C., Thomson R. S., Degenhardt R., Büsing S., Bayandor J. | Development of a Finite Element Methodology for Modelling Mixed-Mode Delamination Growth in Composite Structures | Proceedings of the 12th Australian International Aerospace Congress | 19-22 March, Melbourne, Australia | ||
| 36 | Degenhardt R., Tessmer J. | New Achievements in Stability of Composite Airframe Structures | Proceedings of the 12th Australian International Aerospace Congress | 19-22 March, Melbourne, Australia | ||
| 35 | Bisagni, C. | Numerical analysis of composite panels in the post-buckling field taking into account progressive failure | Proceeding of the International Conference on Computational and Experimental Engineering and Sciences - ICCES '07 | 3-8 Jan., Miami, USA | ||
| 2006 | ||||||
| 34 | Zimmermann R., Klein H., Kling A. | Buckling and Postbuckling analysis of stringer stiffened fibre composite curved panels | Composite Structures, Vol. 73 | pp. 150-161 |
||
| 33 | Kling A., Degenhardt R., Zimmermann R. | A Hybrid Subspace Analysis Procedure for Non-Linear Postbuckling Calculation | Composite Structures, Vol. 73 | pp. 162-170 |
||
| 32 | Wagner, W., Balzani, C. | Simulation of Delamination in Stringer Stiffened Fiber-Reinforced Composite Shells | submitted to Computers & Structures |
|||
| 31 | Wagner, W., Balzani, C. | Finite Element Simulation of Skin-Stiffener Debonding in Curved Fiber-Reinforced Shell Structures | International Workshop Research in Mechanics of Composites 2006 | 26-29 Nov., Bad Herrenalb, Germany | ||
| 30 | Degenhardt R. | Future Design for Composite Airframe Structures – The Projects POSICOSS and COCOMAT | 4th International Conference on New Aerospace Trends | 26-27 October, Bilbao, Spain | ||
| 29 | Kling, A., Degenhardt, R., Zimmermann, R. | A Hybrid Subspace Analysis Procedure for Non-Linear Postbuckling Calculation | Composite Structures, Vol. 73 (2006) | pp. 162-170 | ||
| 28 | Rohwer, K., Degenhardt, R. | COCOMAT - ein EU-Projekt zur Simulation des Beulverhaltens geschädigter Schalen aus Faserverbundmaterial | Jubiläum der Zeitschrift Technische Mechanik, 22. September, 2006 |
|||
| 27 | Balzani, C., Wagner, W. | Analysis of delamination and skin-stringer separation in uni-directional carbon-fiber-reinforced shell structures | CDCM06 – Conference on Damage in Composite Materials: Simulation and Non-Destructive Testing | 18-19 Sept., Stuttgart, Germany | ||
| 26 | Bisagni, C., Cordisco, P., Abramovich, H., Weller, T. | Cyclic buckling tests of CFRP curved panels | Proceedings of the 25th Congress of International Council of the Aeronautical Sciences | pp. 1-8 | 3-8 September, Hamburg, Germany | |
| 25 | Kling, A., Degenhardt, R., Zimmermann, R. | A Flexible Subspace Analysis Procedure for Non-linear Calculations | Proceedings of the 25th Congress of International Council of the Aeronautical Sciences | 3-8 September, Hamburg, Germany | ||
| 24 | Degenhardt, R., Kling, A., Rohwer, K. | Future Design Scenario for Composite Airframe Panels | Proceedings of the 25th Congress of International Council of the Aeronautical Sciences | 3-8 September, Hamburg, Germany | ||
| 23 | Wagner, W., Balzani, C. | Modeling of Skin-Stringer Separation with Cohesive Zone Elements in Fiber-Reinforced Composite Shells | 7th World Congress on Computational Mechanics | 16-22 July, Los Angeles, USA | ||
| 22 | Orifici, A. C., Thomson, R. S., Degenhardt, R., Bisagni, C. Bayandor, J. | Development of a degradation model for the collapse analysis of composite aerospace structures | XIV International Conference on Mechanics of Composite Materials | May 29 - June 2, Riga, Latvia |
||
| 21 | Degenhardt, R. | Improved Exploitation of Composite Airframe Structures by Accurate Simulation of Collapse – The COCOMAT project | Aeronautics Days | 19-21 June, Vienna, Austria | ||
| 20 | Orifici, A. C., Thomson, R. S., Degenhardt, R., Bisagni C., Bayandor, J. | Development of a Degradation Model for the Collapse Analysis of Composite Aerospace Structures | Proceedings of the III European Conference on Computational Mechanics | 5-8 June, Lisbon, Portugal | ||
| 19 | Degenhardt, R., Kling, A., Rohwer, K. | Design and Analysis of Composite Panels | Proceedings of the III European Conference on Computational Mechanics | 5-8 June, Lisbon, Portugal | ||
| 18 | Wagner, W., Balzani, C. | Simulation of Delamination in Stringer Stiffened Fiber-Reinforced Composite Shells | Proceedings of the III. European Conference on Computational Solid and Structural Mechanics | 5-8 June, Lisbon, Portugal | ||
| 17 | Degenhardt, R., Rolfes, R., Zimmermann, R., Rohwer, K. | COCOMAT - improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapse | Composite Structures, Volume 73, Issue 2 , May 2006 |
Pages 175-178 |
Abstract | |
| 16 | Bisagni, C. | Progressive delamination analysis of stiffened composite panels in post-buckling | Proceedings of the 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Material Conference | AIAA 2006-2178, pp. 1-12 | 1-4May, Newport, Rhode Island, USA | |
| 15 | Gleiter A., Riegert G., Zweschper Th., Degenhardt R., Busse G. | Advanced ultrasound activated Lockin-Thermography for defect selective depth resolved imaging | 28th Thermosense Conference | 17-20 April, Orlando, USA | ||
| 14 | Balzani, C., Wagner, W. | Delamination Analysis of UD Composites Using Interface Elements | PAMM – Proc. Appl. Math. Mech. 6, (2006) | 151-152 | full text | |
| 2005 | ||||||
| 13 | Degenhardt R., Tessmer J. | Advances in Computational Stability Analysis of Composite Aerospace Structures | Int. Congress on FEM Technology - 23rd CADFEM Users’ Meeting | 9-11 November, Bonn, Germany | ||
| 12 | Orifici, A.C., Thomson, R.S., Degenhardt, R., Kling, A., Rohwer, K., Bayandor, J. | Degradation Investigation in a Postbuckling Composite Stiffened Fuselage Panel | 13th International Conference on Composite Structures (ICCS-13) |
14-16 November, Melbourne, Australia | Download | |
| 11 | Gruttmann, F., Wagner, W. | Structural analysis of composite laminates using a mixed hybrid shell element | Computational Mechanics 37 (2006) | 479-497 | DOI | |
| 10 | Balzani, C., Wagner, W. | An Interface Element for the Simulation of Delamination in Uni-Directional Fiber-Reinforced Composite Laminates | EUROMECH Colloquium 473: Fracture of Composite Materials | 27-29 October, Porto, Portugal | ||
| 9 | Orifici, A. C., Thomson, R. S., Gunnion, A. J., Degenhardt, R., Abramovich, H., Bayandor, J. |
Benchmark Finite Element Simulations of Postbuckling Composite Stiffened Panels | 11th Australian International Aerospace Congress | 13-17 March, Melbourne, Australia | Abstract | |
| 8 | Degenhardt, R., Zimmermann, R., Rolfes R., Rohwer K. | Improved Material Exploitation of Composite Airframe Structures by Accurate Simulation of Postbuckling and Collapse - The projects POSICOSS and COCOMAT | 11th Australian International Aerospace Congress | 13-17 March, Melbourne, Australia | Abstract | |
| 7 | Balzani, C., Wagner, W | A Simple Model for the Simulation of Delamination in Fibre-Reinforced Composite Laminates under Mixed-Mode Loading Conditions | PAMM - Proc. Appl. Math. Mech. 5, 2005 | 325-326 | 2005 | full text |
| 6 | Gruttmann, F., Wagner, W. | Finite-Element-Modellierungen von Faserverbundstrukturen | 11. Nationales Symposium SAMPE Deutschland e.V., Faser-Kunststoff-Verbunde - neue Freiheitsgrade in der Konstruktion | 1-14 | 3-4 March, Darmstadt, Germany | |
| 2004 | ||||||
| 5 | Wagner, W., Gruttmann, F. | On Efficient FE-Formulations in the Stability Analysis of Thin-walled Structures | 6th World Congress on Computational Mechanics (WCCM VI) | Paper 509, 1-10 | 05-10 September, Beijing, China | |
| 4 | Auzins, J. | Direct Optimization of Experimental Designs | 10th AIAA/ISSMO Multidisciplinary Analysis and Optimizatio Conference | 30 August - 1 September, Albany, New York, USA |
||
| 3 | Wagner, W., Gruttmann, F. | A new stabilized one-point integrated shear-elastic plate element | 4th European Congress on Computational Methods in Applied Sciences and Engineering | Paper 350, 1-13 | 24-28 July, Jyväskylä, Finland | |
| 2 | Rikards, R. | Surrogate Modelling in Design Optimiztion of Stiffened Composite Shells | 4th European Congress on Computational Methods in Applied Sciences and Engineering | 24-28 July, Jyväskylä, Finland | ||
| 1 | Degenhardt, R., Rolfes, R., Zimmermann, R., Rohwer, K. |
Improved Material Exploitation at Safe Design of Composite Airframe Structures by Accurate Simulation of Collapse | International Conference on Buckling and Postbuckling Behaviour of Composite Laminated Shell Structures |
1-2 March, Eilat, Israel |
Abstract | |