Robust knockdown factors for the design of axially loaded cylindrical and conical composite shells – Development and Validation-Reference-Cited by-同舟云学术

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Robust knockdown factors for the design of axially loaded cylindrical and conical composite shells – Development and Validation

Published:2017-08 Issue: Volume:173 Page:281-303
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Wagner H.N.R.,Hühne C.,Niemann S.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference68 articles.

1. Elastic stability of thin-walled cylindrical and conical shells under axial compression;Weingarten;AIAA J,1965

2. Peterson JP, Seide P, Weingarten VI, Buckling of thin-walled circular cylinders - NASA SP-8007, Technical Report; 1 Aug 1968.

3. Weingarten V, Seide P, NASA SP-8019 – buckling of thin-walled truncated. NASA space vehicle design criteria; 1968.

4. A. R. 2A, Recommended practise for planning, designing and constructing fixed offshore platforms. American Petroleum Institute; 2003.

5. D.-R. Recommended Practise, Buckling strength analysis. Det Norske Veritas; 2013.

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