Mixed-mode crack propagation of stiffened curved panels repaired by composite patch under combined tension and shear cyclic loading-Reference-Cited by-同舟云学术

Mixed-mode crack propagation of stiffened curved panels repaired by composite patch under combined tension and shear cyclic loading

Published:2013-07 Issue:1 Volume:28 Page:344-363
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hosseini-Toudeshky Hossein,Ghaffari Mir Ali,Mohammadi Bijan

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Crack patching;Baker,1988

2. A.A. Baker, Fatigue crack propagation studies on aluminum panels patched with boron/epoxy composite, in: R. Jones, N.J. Miller (Eds.), International Conference on Aircraft Damage Assessment and Repair, Melbourne, Australia, 1991, pp. 209–15.

3. Bonded composite repair of fatigue-cracked primary aircraft structure;Baker;Compos. Struct.,1999

4. Fatigue crack growth in stiffened panels under pressure loading-design of fatigue and fracture resistant structures;Chu;ASTM STP,1982

5. Mixed-mode fatigue crack growth in aluminium plates with composite patches;Chung;Int. J. Fatigue,2003

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