Buckling analysis of skew laminate plates subjected to uniaxial inplane loads-Reference-Cited by-同舟云学术

Buckling analysis of skew laminate plates subjected to uniaxial inplane loads

Published:2000-09 Issue:1 Volume:38 Page:53-77
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

Hu H.-T.,Tzeng W.-L.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference20 articles.

1. Buckling analysis of laminated composite plates;Crouzet-Pascal;Fibre Science and Technology,1978

2. Optimum design of laminated plates under axial compression;Hirano;AIAA Journal,1979

3. Effects of orthotropy and width on the compression strength of graphite–epoxy panels with holes;Rhodes;AIAA Journal,1984

4. Leissa AW. Buckling of laminated composite plates and shell panels. AFWAL-TR-85-3069, Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright–Patterson Air Force Base, Ohio, 1985.

5. Optimal fibre orientation for simply-supported angle-ply plates under biaxial compression;Muc;Composite Structures,1988

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