The computational post buckling analysis of fuselage stiffened panels loaded in compression-Reference-Cited by-同舟云学术

The computational post buckling analysis of fuselage stiffened panels loaded in compression

Published:2004-10 Issue:10 Volume:42 Page:1445-1464
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

Lynch C.,Murphy A.,Price M.,Gibson A.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference18 articles.

1. Airframe structural design;Niu,1988

2. Lynch CJ. A finite element study of the post buckling behaviour of a typical aircraft fuselage panel. PhD Thesis, Queen’s University Belfast, Belfast, Northern Ireland, 2000.

3. NASA. NASA astronautics structures manual, vol. 3. NASA, Washington, US, 1961.

4. ESDU structures sub-series, Engineering Sciences Data Units, ESDU International Ltd.

5. Airframe stress analysis and sizing;Niu,1999

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