EXPERIMENT AND SIMULATION RESEARCH ON UNIFORM SUPERCHARGED FATIGUE CRACK INITIATION OF AIRCRAFT FUSELAGE SKIN

The fatigue crack initiation of the fuselage structure skin under the uniform supercharged cyclic load of 0 ~ 7. 8 Psi was experimentally studied by the self-made aircraft fuselage skin uniform supercharged fatigue simulation device. The location of the fatigue crack initiation of the fuselage struc...

詳細記述

書誌詳細
主要な著者: LIU LiPing, ZHANG Fang, ZHONG XiaoKun, BAO Rui, XU JianXin, QIN WenChao
フォーマット: 論文
言語:zho
出版事項: Editorial Office of Journal of Mechanical Strength 2020-01-01
シリーズ:Jixie qiangdu
主題:
オンライン・アクセス:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2020.04.032