Initial buckling of curved panels of generally layered composite materials-Reference-Cited by-同舟云学术

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Initial buckling of curved panels of generally layered composite materials

Published:1983-01 Issue:1 Volume:1 Page:3-30
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Zhang Y.,Matthews F.L.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference10 articles.

1. Theory of laminated plates;Ashton,1970

2. Mechanics of composite materials;Jones,1975

3. Theoretical buckling loads of boron/aluminium and graphite/resin fibre—Composite anisotropic plates;Chamis;NASA TN D-6572,1975

4. Analysis of simply supported laminated anisotropic rectangular plate;Whitney;AIAA Journal,1970

5. Composite materials and their use in structures;Vinson,1975

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1. The effects of surroundings and stiffeners in the CUF-based postbuckling analysis of composite panels under in-plane shear;Mechanics of Advanced Materials and Structures;2022-05-19

2. Stability of Plates and Shell Panels Under Non-uniform In-Plane Loadings;Composites Science and Technology;2022

3. Design of curved composite panels for maximum buckling load using sequential permutation search algorithm;Structures;2021-12

4. Buckling and postbuckling of rotationally-restrained laminated composite plates under shear;Thin-Walled Structures;2021-04

5. Buckling analysis of composite laminated plate in different boundary conditions under thermo mechanical loading;Materials Today: Proceedings;2021

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