The behaviour of damage tolerant hat-stiffened composite panels loaded in uniaxial compression-Reference-Cited by-同舟云学术

The behaviour of damage tolerant hat-stiffened composite panels loaded in uniaxial compression

Published:2001-09 Issue:9 Volume:32 Page:1255-1262
ISSN:1359-835X
Container-title:Composites Part A: Applied Science and Manufacturing
language:en
Short-container-title:Composites Part A: Applied Science and Manufacturing

Author:

Falzon Brian G.

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference22 articles.

1. Starnes Jr JH, Knight NF, Rouse M. Postbuckling behavior of selected flat stiffened graphite-epoxy panels loaded in compression. AIAA J Paper 82-0777, 1982. p. 464–78.

2. Buckling and postbuckling of composite structures;Stevens;Composites,1995

3. Falzon BG, Stevens KA, Goia M, Davies GAO. Postbuckling failure of a blade-stiffened carbon-epoxy compression panel. In: 12th International Conference on Composite Materials (ICCM-12), 5–9 July 1999, Paris, France.

4. Experimental investigation on advanced composite-stiffened structures under uniaxial compression and bending;Romeo;AIAA J,1986

5. Brooks WG. The design and construction of a post buckled carbon fibre wing box structure, ICAS-86-4.2.1, 1986. p. 238–43.

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