Aircraft fatigue life extension: Development of a mid-life rework method based on peening-Reference-Cited by-同舟云学术

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Aircraft fatigue life extension: Development of a mid-life rework method based on peening

Published:2000 Issue: Volume: Page:97-114
ISSN:1566-1369
Container-title:Fracture Mechanics: Applications and Challenges, 13th European Conference on Fracture
language:
Short-container-title:

Author:

Clark G.

Publisher

Elsevier

Reference12 articles.

1. Accident and Failure Analysis: Learning from Experience;Cox,1989

2. Analysis and Interpretation of Aircraft Component Defects Using Quantitative Fractography;Goldsmith,1990

3. Repair of cracked or defective metallic components with advanced fibre composites—an overview of Australian work;Baker;Composite Structures,1984

4. Cyclic Growth and Coalescence of Multiple Fatigue Cracks;Grandt,1984

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Crack Growth Prediction on Critical Component for Structure Life Extension of Royal Malaysian Air Force (RMAF) Sukhoi Su-30MKM;Metals;2021-09-14

2. Crack Propagation Behaviour in Thin Aluminium Alloy Sheet Repaired with Adhesively Bonded CFRP Patch;Transactions of the Indian Institute of Metals;2019-11-29

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