Recent Developments in the Design, Testing and Impact-Damage Tolerance of Stiffened Composite Panels

This publication has 5 references indexed in Scilit:

• Effect of Impact Damage and Holes on the Compressive Strength of a Graphite/Epoxy Laminate
  Published by ASTM International ,1979
• A general panel sizing computer code and its application to composite structural panels
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1978
• Buckling Behavior and Structural Efficiency of Open-Section Stiffened Composite Compression Panels
  AIAA Journal, 1976
• Analytical and experimental study of structurally efficient composite hat-stiffened panels loaded in axial compression
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1975
• Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadings
  International Journal of Mechanical Sciences, 1974