Effects of shear loads on vibration and buckling of antisymmetric cross-ply cylindrical panels-Reference-Cited by-同舟云学术

Effects of shear loads on vibration and buckling of antisymmetric cross-ply cylindrical panels

Published:1988-01 Issue:3 Volume:23 Page:177-187
ISSN:0020-7462
Container-title:International Journal of Non-Linear Mechanics
language:en
Short-container-title:International Journal of Non-Linear Mechanics

Author:

Hui David

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials

Reference20 articles.

1. Design of composite material structures for buckling-an evaluation of the state-of-the-art.;Almroth;U.S. Air Force Wright Aeronautical Laboratory, Technical Report AFWAL-TR-81-3102,1981

2. Imperfection sensitivity of optimized structures;Almroth;U.S. Air Force Wright Aeronautical Laboratory, Technical Report AFWAL-TR-80-3128,1981

3. Buckling of composite plates;Leissa;Comp. Struct.,1983

4. A.W. Leissa, Buckling of laminated composite plates and shell panels, AFWAL-TR-85-306.

5. Mechanics of Composite Materials;Jones,1975

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