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Compressive and shear buckling analysis of metal matrix composite sandwich panels under different thermal environments

  • Published:1993-01 Issue:1-4 Volume:25 Page:227-239
  • ISSN:0263-8223
  • Container-title:Composite Structures
  • language:en
  • Short-container-title:Composite Structures

Author:

Ko William L.,Jackson Raymond H.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference9 articles.

1. Metal Matrix Composites: Thermomechanical Behavior;Taya,1989

2. Materials and structures for hypersonic vehicles;Tenny;J. Aircraft,1989

3. Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels;Ko;NASA TM-4290,1991

4. AIAA paper no. 92-2478-CP, presented at the 33rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference,1992

5. Uniaxial compressive and shear buckling in orthotropic sandwich plates by improved theory;Bert;AIAA 86–0977,1986

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