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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| Asıl Yazarlar: | , , , , |
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| Materyal Türü: | Artigo |
| Dil: | Chinês |
| Baskı/Yayın Bilgisi: |
Editorial Office of Journal of Mechanical Strength
2025-11-01
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| Seri Bilgileri: | Jixie qiangdu |
| Konular: | |
| Online Erişim: | http://www.jxqd.net.cn/thesisDetails#DOI：10.16579/j.issn.1001.9669.2025.11.013 |
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