Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime-Reference-Cited by-同舟云学术

Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime

Published:1993-03 Issue:1-2 Volume:103 Page:43-114
ISSN:0045-7825
Container-title:Computer Methods in Applied Mechanics and Engineering
language:en
Short-container-title:Computer Methods in Applied Mechanics and Engineering

Author:

Bushnell David

Publisher

Elsevier BV

Subject

Computer Science Applications,General Physics and Astronomy,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference69 articles.

1. Buckling of laminated composite plates and shell panels;Leissa,1985

2. Postbuckling of thin-walled composite structures — Design, analysis, and experimental verification;Wiggenraad,1986

3. Buckling, postbuckling, and failure of flat and shallow-curved, edge-stiffened composite plates subject to combined axial compression and shear loads;Arnold,1986

4. PANDA-Interactive program for minimum weight design of stiffened cylindrical panels and shells;Bushnell;Comput. & Structures,1983

5. Theoretical basis of the PANDA computer program for preliminary design of stiffened panels under combined in-plane loads;Bushnell;Comput. & Structures,1987

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