List of all Abstracts

1	DLR, ACARE, Germany	J. Szodruch	Future Aircraft Technologies - The European Strategic Research Agenda
2	Airbus, Germany	P. Linde	Overview of Test Prediction and Damage Simulation of Composite Aircraft Structures
3	DLR, PFH Goettingen,Germany	R. Degenhardt, D. Wilckens, K. Rohwer, R. Zimmermann, J. Tessmer	Improved Material Exploitation of Composite Airframe Structures by Accurate Simulation of Collapse - The COCOMAT project
4	SMR, Switzerland	E. Riks	On the Purpose and Limitations of Buckling Analysis
5	TU Delft, Netherlands,	J. Arbocz, J.de Vries	Looking for alternate ways to define Knockdown Factors
6	DLR, Germany	J. Tessmer	Structural Mechanics in the Design Process of Composite Aircraft Structures
7	NASA, USA	M. Hillburger	Developments in Shell Buckling Analysis, Design and Testing
8	Germany	R. Cuntze	Formulations of Failure Conditions - Isn't it basically just Beltrami and Mohr-Coulomb?
9	EADS Astrium Space, Germany	A. Rittweger, S. Christianson, H. Oery	Dimensioning of Orthotropic Stiffened CFRP Shells of Large Launch Vehicle for Load Introduction and Stability
10	ESA, Netherlands	A. Calvi	E.C.S.S. Buckling handbook
11	Airbus, Germany	M. Schagerl	HSB - A Handbook for Fundamentals and Methods for Aeronautical Design and Analyses
12	Leibnitz University Hannover, Germany	C. Huehne, M. Vogler, G. Ernst, R. Rolfes	Multiscale Approach for Determination of Stiffness and Strength of Textile Composites
13	DLR, Germany	R. Degenhardt, D. Wilckens, K. Rohwer, M. Kepke, B. Hildebrandt, A. Zipfel	Buckling and collapse tests using advanced measurement systems
14	DLR, Germany; Airbus, Germany	D. Wilckens, R. Degenhardt, K. Rohwer, J. Tessmer, P. Buermann	IBUCK - A fast simulation tool for the design of CFRP aerospace structures
15	Agusta-Westland, Italy; DLR, Germany	A. Caruso, V. Pietroni, E. Masiero, R. Degenhardt	Material properties, design of structures and degradation models
16	Aernnova, Spain	J. A. Araico, I. Ortiz de Zarate Alberdi, F.R. Arribas	FEM Simulation of Potted-Ends on Compression Loaded Graphite-Epoxy Test Specimens
17	Aernnova, Spain; TECHNION, Israel	H. Abramovich, T. Weller, I. Ortiz de Zarate Alberdi	Experimental results on buckling and postbuckling behavior of panels - An overview
18	HAI, Greece; POLIMI, Italy; Aernnova, Spain; Agusta, Italy	C. Vrettos, E. Karachalios, Z. Marioli-Riga, C. Bisagni, P. Cordisco, A. Caruso, I. Ortiz de Zarate Alberdi	Non-Linear analysis of stiffened composite boxes under combined loading
19	IAI, Israel	G. Ghilai, E. Feldman, A. David	COCOMAT Guidelines for design & analysis of CFRP stiffened panels for buckling & postbuckling
20	PZL, Poland	M. Zeglen, P. Chojnacki, J. Ogiela	Participation, results and experiences from the COCOMAT project
21	SAMTECH, Belgium	M. Bruyneel, B. Colson, J.P. Delsemme, J.P. Jetteur, P. Morelle, A. Remouchamps	Exploiting semi-analytical sensitivities from linear and nonlinear finite-element analyses for composite panel optimization
22	SMR, Switzerland	M. Doreille, S. Merazzi	Post-buckling analysis of composite structures with B2000++
23	CRC-ACS, Australia; DLR, Germany; POLIMI, Italy	A. Orifici, R.S. Thomson, R. Degenhardt, C. Bisagni, J. Bayandor	An analysis tool for design and certification of postbuckling composite aerospace structures
24	CRC-ACS, Australia; TECHNION, Israel	A. Orifici, I. Herszberg, A. Kotler, R.S. Thomson, J. Bayandor, H. Abramovich, T. Weller	Failure in skin-stiffener sections under postbuckling loads
25	CRC-ACS, Australia; TECHNION, Israel; UKA, Germany	A. Orifici, S. Lauterbach, H. Abramovich, R.S. Thomson, W. Wagner, C. Balzani	Analysis of damage sensitivity and collapse in postbuckling fibre-reinforced multi-stiffener panels
26	FOI, Sweden	R. Jarlas	A benchmark example for collapse analysis of stiffened composite panels
27	UKA, Germany	C. Balzani, W. Wagner	Numerical Treatment of Damage Propagation in Axially Compressed Composite Airframe Panels
28	POLIMI, Italy	P. Cordisco, C. Bisagni	Cyclic buckling of composite boxes
29	RTU, Latvia; POLIMI,Italy; TECHNION, Israel	K. Kalnins, R. Rikards, J. Auzins, C. Bisagni, H. Abramovich	Metamodeling methodology for post-buckling simulation of composite stiffened structures with physical validation
30	RTU, Latvia; DLR, Germany	R. Rikards, K. Kalnins, R. Degenhardt	Overview of slow computational and fast simulation tools
31	RWTH, Germany	H. Reimerdes, S. Buesing	Failure and Failure Progression in the Skin-Stiffener Interface in Composite Specimens
32	RWTH, Germany	S. Buesing, H. Reimerdes, T. Moecker	Simulation of Postbuckling Experiments with a Fast Design Tool
33	RWTH, Germany	S. Buesing, H. Reimerdes	A Strip Element with Interface Layer for the Prediction of Delamination in Buckled Composite Panels
34	TECHNION, Israel; POLIMI, Italy	H. Abramovich, C. Bisagni, P. Cordisco	Effect of cyclic post-buckling loads on cfrp panels
35	TECHNION, Israel	H. Abramovich, T. Weller	Repeated Buckling and Postbucking Behavior of Laminated Stringer Stiffened Composite Panels with and without Damage
36	TECHNION, Israel	H. Abramovich, T. Weller	Buckling and Postbucking Behavior of Laminated Composite Stringer Stiffened Curved Panels under Axial Compression-Experiments and Design
37	Cardiff University, UK	C.A. Featherston, D. Kennedy, S. Qu	Multi-level postbuckling optimum design of aerospace structures
38	Imperial College, UK	C. Voellmecke, M. A. Wadee	Nonlinear buckling of uniaxially compressed delaminated composite panels
39	QinetiQ, UK	C. Williamson, S. J. Lord	Damage prediction and its effect on post-buckled wing design
40	University College London, UK	H. Wang, J.G.A. Croll	Finite element validation of a lower-bound design method for optimising buckling capacities of FRP shells
41	University of Bristol, UK	J.E. Herencia, P.M. Weaver, M.I. Friswell	A fast optimization technique for preliminary sizing of anisotropic composite stiffened panels
42	University_Naples, Italy	C. Meola, G. Carlomagno, M. Valentino, C. Bonavolonta	Non destructive evaluation of impact damage in cfrp with infrared thermography and squid
43	TU Delft, Netherlands	T. Rahman, E.L. Jansen	Finite element based coupled mode initial post-buckling analysis of a composite cylindrical shell
44	TU Lisbon, Portugal; DLR, Germany	N. Silva, D. Camotim, N. Silvestre, R. Degenhardt	Application of generalised beam theory to the study of the stability behaviour of laminated CFRP cylindrical stiffened panels
45	University of Innsbruck, Austria,	M. Oberguggenberger, J. King	Buckling and collapse of shell structures: sensitivity analysis
46	IAI, Israel	V. Weissberg, T. Genosar, G. Ghilai	Instability and collapse of sandwich shells; representing a/c wing skins
47	Univeristy of New South Wales, Australia; CRC-ACS, Australia; DLR, Germany	M.C.W. Lee, R.S. Thomson, R. Degenhardt, D.W. Kelly	A stochastic study on the robustness of a stiffened composite structure
48	CRC-ACS, Australia	Z. Mikulik, R.S. Thomson, D.W. Kelly, B.G. Prusty	Assessment of fracture mechanics based methodologies to predict skin-to-stiffener debonding in a postbuckling compression panel
49	ASRI, China	C.L. Wu	Buckling Behaviour of Composite Laminated Corrugated Panel with Sinusoidal Profile First Part: Equivalent Stiffness Terms
50	ASRI, China; UKA, Germany; DLR, Germany	H. Wang, X. Sun, A. Bueschel, W. Wagner, R. Degenhardt, K. Rohwer	Empirical formula for the critical perturbation load
51	SAMTECH, Belgium	C. Brauner, Y. Radovcic, J.P. Delsemme, P. Jetteur	Advanced non linear failure analysis of a reinforcement composite curved beam with delamination and ply degradation
52	DLR, Germany	J. Orf, L. Kaerger, R. Degenhardt, A. Bethge	The influence of imperfections on the buckling behavior of unstiffened CFRP-cylinders
53	Ferchau, DLR, Germany	A. Wetzel, J. Baaran	Residual strength prediction of impacted composite sandwich structures
54	Airbus, Germany; DLR, Germany	P. Steinmueller, R. Degenhardt, K. Rohwer	Investigations of axially loaded unstiffened CFRP cylindrical shells subject to single perturbation loads
55	PFH Goettingen, Airbus, Germany,	C. Mittelstedt, M. Beerhorst	Closed-form buckling analysis of omegastringer-stiffened composite panels considering periodic boundary conditions
56	PFH Goettingen, Airbus, Germany	C. Mittelstedt, M. Schagerl	The Windenburg problem revisited: Buckling and minimum stiffness requirements for composite plates with reinforced edges
57	FH Hanover, CADFEM, Germany	W. Rust, M. Kracht	Recent experiences in load analysis of aircraft fuselage panels
58	EADS-MAS, Germany	G. Schuhmacher, M. Wagner, A. Hoermann, F. Daoud	Optimisation of Composite Aircraft Structures in Consideration of Postbuckling Behaviour
59	LUH Hannover, Germany	C. Huehne, R. Rolfes	Probabilistic approach to determine the lower limit of buckling load of composite shells
60	Abaqus, Bishop, Airbus, Germany	T. Moecker, F. Goetz, J. Marsolek, S. Kraschin, P. Linde, W. Wohlers	Abaqus FEM Analysis of the Postbuckling Behaviour of Composite Shell Structures
61	TU Braunschweig, Germany	J. Pontow, D. Dinkler	Evaluation of the perturbation sensitivity of composite laminated shells
62	Alpha STAR, USA	F. Abdi, D. Huang	Progressive fracture of stitched stiffened composite shear panels in the post buckling range
63	NASA, USA	C.C. Chamis	Dynamic Buckling of Thin Composite shells
64	Alenia, Italy	B. Gambino	Methodology to analyze postbuckling behaviour for multispar configuration structures
65	Beihang University, China	H. Wu, Y. Ya	A Parametric Study for the Design of Stiffened Composite Panels