FATIGUE LIFE ANALYSIS OF SIMULATED AIRCRAFT BEAM STRUCTURE CONNECTION

Experimental and simulation methods were used to predict the fatigue life of the connecting part of the aircraft beam structure. First of all,based on the statistical analysis,the marker load was chosen. The experimental results show that the marker load method can quantitatively record the initiati...

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Detalhes bibliográficos
Main Authors: ZHENG Jie, LIU Yang, TONG MingBo
Formato: Artigo
Idioma:zho
Publicado em: Editorial Office of Journal of Mechanical Strength 2020-01-01
Colecção:Jixie qiangdu
Assuntos:
Acesso em linha:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2020.01.029