Postbucking behaviour of a blade-stiffened composite panel loaded in uniaxial compression

Composites Part A: Applied Science and Manufacturing

Volumn 31, Issue 5, 2000, Pages 459-468

  Falzon, B G ^a   Stevens, K A ^a   Davies, G O ^a  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BENDING (DEFORMATION); BUCKLING; CALCULATIONS; DELAMINATION; EPOXY RESINS; FAILURE ANALYSIS; LAMINATING; MATERIALS TESTING; SHEAR STRESS; STIFFNESS; STRAIN GAGES;

INTERLAMINAR SHEAR STRESS; STIFFENED COMPOSITE PANEL; THREE POINT BENDING TEST;

CARBON FIBER REINFORCED PLASTICS;

EID: 0033901360     PISSN: 1359835X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1359-835X(99)00085-8     Document Type: Article

References (15)

1. Starnes J.H. Jr., Knight F.K. Jr., Rouse M. Postbuckling behaviour of selected flat stiffened graphite epoxy panels loaded in uniaxial compression. AIAA. 23:(8):1988;344-352.
2. Buskell N, Davies GAO, Stevens KA. Postbuckling failure of composite panels. Proceedings of the Third International Conference on Composite Structures, Paisley, UK, 1985. p. 290.
3. Falzon BG, Steven GP. Postbuckling behaviour of hat-stiffened thin-skinned carbon-fibre composite panels, AIAA/ASME/AHS/ASC 36th Structures, Structural Dynamics and Materials Conference, New Orleans, LA, USA, 1995.
4. Stevens KA, Specht S, Davies GAO. Postbuckling failure of carbon-epoxy compression panels, Proceedings of ICCM-11, Gold Coast, Australia, 1997.
5. Stevens K.A., Ricci R., Davies G.A.O. Buckling and postbuckling of composite structures. Composites. 26:(3):1995;189-199.
6. Stevens KA, Davies GAO, Ricci R. Postbuckling failure of composite compression panels. 19th ICAS Conference, ICAS-94-9.8.3, Anaheim, California, 1994. p. 2975-81.
7. Singer J., Arbocz J., Weller T. Experimental methods in buckling of thin-walled structures - volume 1 Buckling experiments. 1998;Wiley, New York.
8. Falzon BG, Hitchings D, Stevens KA, Davies GAO. Failure prediction of thick structural composites, Progress Report 3, DTI CARAD Contract DTI/SMC/4/968, Imperial College of Science, Technology and Medicine, London, 1998.
9. Hitchings D. FE77 User Manual, Imperial College of Science, Technology and Medicine, 1994.
10. Falzon B.G., Steven B.G. Buckling mode transition in hat-stiffened composite panels loaded in uniaxial compression. Composite Structures. 37:1998;253-267.
11. Bushnell D., Rankin C.C., Riks E. Optimization of stiffened panels in which mode jumping is accounted for. AIAA paper. 97-1141:1998;105-145.
12. Jones R.M. Mechanics of composite materials. 1975;McGraw-Hill, New York.
13. Kretsis G. Laminate Analysis Program, LAP, Centre for Composite Materials, Imperial College of Science, Technology and Medicine, London, 1995.
14. Davies GAO, Buskell N, Stevens KA. Edge effects in failure of compression panels, Euromech 214 Symposium on Composites, Amsterdam, 1986.
15. Davies G.A.O. Virtual work in structural analysis. 1982;Wiley, New York.