Author:
Barut Atila,Madenci Erdogan
Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. 1Owen V. and Klang F. "Shear Buckling of Specially Orthotropic Plates with Centrally Located Cutouts," 8th DOD/NASA/FAA Conference on Fibrous Composites in Structural Design, Part 2, Norfolk, Virginia, NASA CP3087,1989.
2. Shear and compression buckling analysis for anisotropic panels with elliptical cutouts
3. 3Jones, K. M. and Klang, F. "Buckling Analysis of Fully Anisotropic Plates Containing Cutouts and Elastically Restrained Edges,"33rdAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference Conference,Dallas,Texas,AIAAPaper92-2279,1992.
4. 4Barut, A., and Madenci, E. "A Complex Potential-Variational Formulation for Buckling Analysis of Flat Laminates with Multiple Cutouts,"42ndAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference,SeattleWashington,AIAA Paper2001-1547,2001.