Postbuckling behavior of selected flat stiffened graphite-epoxy panels loaded in compression

This publication has 9 references indexed in Scilit:

• Postbuckling and failure characteristics of selected flat rectangular graphite-epoxy plates loaded in compression
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1981
• Design of Stiffened Composite Panels in the Post-Buckling Range
  Published by Springer Nature ,1980
• A PRELIMINARY DESIGN PROCEDURE FOR COMPOSITE PANELS WITH OPEN-SECTION STIFFENERS LOADED IN THE POST-BUCKLING RANGE
  Published by Elsevier ,1980
• Effect of Impact Damage and Holes on the Compressive Strength of a Graphite/Epoxy Laminate
  Published by ASTM International ,1979
• General Panel Sizing Computer Code and Its Application to Composite Structural Panels
  AIAA Journal, 1979
• Buckling and post-buckling of orthotropic laminated plates
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1975
• The buckling and post-buckling behaviour of composite plates under biaxial loading
  International Journal of Mechanical Sciences, 1975
• Evaluation of various analytical models for buckling and vibration of stiffened shells.
  AIAA Journal, 1973
• The Large Deflection and Post-Buckling Behaviour of Some Laminated Plates
  Aeronautical Quarterly, 1973