Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch-Reference-Cited by-同舟云学术

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Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch

Published:1997-07 Issue:5 Volume:57 Page:507-525
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Denney J.J.,Mall S.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference13 articles.

1. Boron/epoxy composites for aircraft structural repair;Caruso;Composite Polymers,1991

2. Today's Aircraft, Flying Tomorrow [Status of the USAF Flight Dynamics Directorate Approach to the USAF Aging Aircraft Problem];Hart,1995

3. Bonded repair of aircraft structures;Ekstrom;Materials Evaluation,1992

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4. Computational assessment of disbond growth behaviour in adhesively bonded wide joints or patch repairs for primary airframe structures;Composites Part C: Open Access;2022-10

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