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Fatigue load optimization and test verification of the full-scale aileron

In the fatigue test of aircraft wing structural components, the fatigue design loads need to be optimized so as to reduce the bending, shear and torsion load errors applied during the test. Firstly, taking the full-scale aileron as the research object, the fatigue test load optimization model was es...

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Main Authors: LIU Lu, LI Wang, ZHANG Wei, LI Miao, WANG Pengfei
Format: Artigo
Language:Chinês
Published: Editorial Office of Journal of Mechanical Strength 2025-11-01
Series:Jixie qiangdu
Subjects:
Fatigue test
Full-scale aileron
Load optimization
Objective function
Online Access:http://www.jxqd.net.cn/thesisDetails#DOI：10.16579/j.issn.1001.9669.2025.11.013
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