Fuselage metal fatigue in large commercial aircraft-Reference-Cited by-同舟云学术

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Fuselage metal fatigue in large commercial aircraft

Published:2012 Issue:1 Volume:1 Page:47
ISSN:1744-9944
Container-title:International Journal of Forensic Engineering
language:en
Short-container-title:IJFE

Author:

Bibel G.

Publisher

Inderscience Publishers

Cited by 3 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. Development and structural analysis on longeron cross sectional area in a flat stiffened panel with a broken central longeron;Materials Today: Proceedings;2021-10

2. Two bay crack arrest capability evaluation for metallic fuselage;IOP Conference Series: Materials Science and Engineering;2018-12-01

3. A Study on the Effect of Crack Stopper for Enhanced Damage Tolerance Behavior of a Fuselage Stiffened Panel;Advances in Structural Integrity;2017-12-27

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