Simplified methods for the buckling analysis of composite multi-spar wing boxes-Reference-Cited by-同舟云学术

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Simplified methods for the buckling analysis of composite multi-spar wing boxes

Published:1994-01 Issue:2 Volume:28 Page:215-223
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Aston G.,Williams F.W.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference6 articles.

1. AV-8B/GR5 Mk 5 airframe composite application;Riley,1986

2. An algorithm for computing critical buckling loads of elastic structures;Wittrick;J. Struct. Mech.,1973

3. Analysis features of VICONOPT, an exact buckling and vibration program for prismatic assemblies of anisotropic plates;Williams,1990

4. Assessment of simple procedures for obtaining lower bound buckling loads;Wiliams,1988

5. Optimum design features of VICONOPT, an exact buckling program for prismatic assemblies of anisotropic plates;Butler,1990

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental and numerical investigation on the failure behavior of multi-spar composite box under bending and shear;Journal of Physics: Conference Series;2023-09-01

2. Towards the Design of a Multispar Composite Wing;Computation;2020-04-09

3. Investigation on a multispar composite wing;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2011-09-30

4. Testing and Analysis of Downscaled Composite Wing Box;Journal of Aircraft;2002-05

5. Design of structures by a splitting method;Computers & Structures;1999-02

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