On the USAF ‘risk of failure’ approach and its applicability to composite repairs to metal airframes-Reference-Cited by-同舟云学术

On the USAF ‘risk of failure’ approach and its applicability to composite repairs to metal airframes

Published:2017-05 Issue: Volume:167 Page:103-111
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Hu W.,Barter S.,Wang J.,Jones R.,Kinloch A.J.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference26 articles.

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3. Fatigue crack growth and damage tolerance;Jones;Fatigue Fract Eng Mater Struct,2014

4. ASTM. Measurement of fatigue crack growth rates. ASTM E647-13, USA; 2013.

5. Implications of the lead crack philosophy and the role of short cracks in combat aircraft;Jones;Eng Fail Anal,2013

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