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

Abstract

 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

Proceedings

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

Proceedings

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

Abstract

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

Presentation