Efficient non-linear idealisations of aircraft fuselage panels in compression-Reference-Cited by-同舟云学术

Efficient non-linear idealisations of aircraft fuselage panels in compression

Published:2004-08 Issue:13-14 Volume:40 Page:1977-1993
ISSN:0168-874X
Container-title:Finite Elements in Analysis and Design
language:en
Short-container-title:Finite Elements in Analysis and Design

Author:

Murphy A.,Price M.,Gibson A.,Armstrong C.G.

Publisher

Elsevier BV

Subject

Applied Mathematics,Computer Graphics and Computer-Aided Design,General Engineering,Analysis

Reference20 articles.

1. E.F. Bruhn, Analysis and Design of Flight Vehicle Structures, 1st Edition, Tri-State Offset Company, 1973.

2. NASA, NASA Astronautics Structures Manual, Vol. 3, 1961.

3. Engineering Sciences Data Units, Structures Sub-Series, ©ESDU International Ltd.

4. C.J. Lynch, A finite element study of the postbuckling behaviour of a typical aircraft fuselage panel. Ph.D. Thesis, Queen's University Belfast, Belfast, N. Ireland, 2000.

5. A. Murphy, Accurate and efficient buckling and post buckling analysis of fuselage panels loaded in shear and compression. Ph.D. Thesis, Queen's University Belfast, Belfast, N. Ireland, 2002.

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