Buckling of VAT Plates Using Energy Methods
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Publisher
American Institute of Aeronautics and Astronautics
Reference26 articles.
1. Use of curvilinear fiber format in composite structure design
2. Variable stiffness composite panels: Effects of stiffness variation on the in-plane and buckling response
3. 3Weaver, P. M., Potter, K. D., Hazra, K., Saverymuthapulle, M. A. R., and Hawthorne, M. T. “Buckling of variable angle tow plates: From concept to experiment,” 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2009.
4. 4Olmedo, R. and Gürdal, Z. “Buckling response of laminates with spatially varying fiber orientations,” Collection of Technical Papers - AIAA/ASME Structures, Structural Dynamics and Materials Conference, No. pt 4, 1993, pp.2261 - 2269.
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