Study on crack propagation behaviors of aircraft internal pressure panels with longitudinal cracks

Crack growth analysis of aircraft fuselage panels is one of the important tasks of aircraft damage tolerance design. In this paper, the crack growth behavior and residual strength characteristics of the internal pressure panel of the aircraft fuselage with longitudinal cracks were analyzed from two...

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Bibliographic Details
Main Authors: QIN JianBo, WANG Feng, LÜ Pin, HOU Cheng, FAN XueLing
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2024-06-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2024.03.006
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