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RESEARCH ON THE FATIGUE CRACK PROPAGATION OF AIRCRAFT FUSELAGE SKIN UNDER UNIFORM PRESSURIZED LOAD (MT)

In order to study the fatigue crack propagation of the fuselage skin under uniform pressurized cyclic load, experiments were carried out with the self-made aircraft fuselage skin uniform pressurized fatigue device. Firstly, the stress intensity factor was calculated by the extended finite element me...

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Detaylı Bibliyografya
Asıl Yazarlar: LIU LiPing, HAN HaoHao, LIU JiaHuan, BAO Rui, LIN YueGuo
Materyal Türü: Artigo
Dil:Chinês
Baskı/Yayın Bilgisi: Editorial Office of Journal of Mechanical Strength 2023-01-01
Seri Bilgileri:Jixie qiangdu
Konular:
Online Erişim:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2023.04.031
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