Influence of secondary damage on flight cycles and inspection interval for an aircraft wing panel-Reference-Cited by-同舟云学术

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Influence of secondary damage on flight cycles and inspection interval for an aircraft wing panel

Published:2020-05-25 Issue:6 Volume:42 Page:
ISSN:1678-5878
Container-title:Journal of the Brazilian Society of Mechanical Sciences and Engineering
language:en
Short-container-title:J Braz. Soc. Mech. Sci. Eng.

Author:

Srivastava Amit Kumar,Arora P. K.,Srivastava Sharad Chandra

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Link

https://link.springer.com/content/pdf/10.1007/s40430-020-02425-z.pdf

Reference27 articles.

1. Yang JN, Donath RC (1983) Statistical fatigue crack propagation in fastener holes under spectrum loading. J Aircr 20(12):1028–1032

2. Skorupa M (1999) Load interaction effects during fatigue crack growth under variable amplitude loading—a literature review. Fatigue Fract Eng Mater Struct 22:905–926

3. Zhang XP, Wang CH, Mai YW (2002) Prediction of short fatigue crack propagation behaviour by characterization of both plasticity and roughness induced crack closures. Int J Fatigue 24:529–536

4. Master FJ, Smith DJ (2001) Predictions of fatigue crack growth in aluminium alloy 2024-T351 using constraint factors. Int J Fatigue 23:93–101

5. Merati A, Eastaugh G (2007) Determination of fatigue related discontinuity state of 7000 series of aerospace aluminum alloys. Eng Fail Anal 14(4):673–685

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