Effects of Elastic Edge Restraints and Prestress on the Buckling Response of Compression-loaded Composite Panels

Author:

Hilburger Mark,Riddick Jaret,Thornburgh Robert,Nemeth Michael

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. Effects of imperfections of the buckling response of composite shells

2. Snell, M. B. and Morley, N. T. "The Compression Buckling Behaviour of Highly Curved Panels of Carbon Fibre Reinforced Plastic," Proceedings of the Fifth International Conference on Composite Materials, ICCMVol.5, 1985,pp.1327-1354.

3. Leissa, A. W. "Buckling of Laminated Composite Plates and Shell Panels," Report AFWAL-TR-85-3069, AF Wright Aeronautical Laboratories, June 1985.

4. Asymmetric postbuckling of symmetrically laminated cross ply, short cylindrical panels under compression

5. A numerical and experimental investigation of the buckling behavior of composite panels

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1. Compression buckling of elastically supported cylindrical shells with Bend/Twist coupling;Composite Structures;2023-04

2. Initial post-buckling of variable-stiffness curved panels;Journal of the Mechanics and Physics of Solids;2014-11

3. Difficulties in Optimization of Imperfect Stiffened Cylindrical Shells;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

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