EXPERIMENT AND SIMULATION RESEARCH ON UNIFORM SUPERCHARGED FATIGUE CRACK INITIATION OF AIRCRAFT FUSELAGE SKIN by LIU LiPing, ZHANG Fang, ZHONG XiaoKun, BAO Rui, XU JianXin, QIN WenChao

Subjects: “…Fuselage skin…”
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Shear Stress Distribution in a Fuselage of an Aircraft by Chidebe Stanley Anyanwu, Tolulope Babawarun

Subjects: “…Fuselage…”
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A new methodology to predict damage tolerance based on compliance via global-local analysis by Gilberto Gomes, Thiago Arnaud A Oliveira, Alvaro Martins Delgado Neto, Luciano Mendes Bezerra

Subjects: “…global-local analysis aircraft fuselage…”
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RESEARCH ON THE FATIGUE CRACK PROPAGATION OF AIRCRAFT FUSELAGE SKIN UNDER UNIFORM PRESSURIZED LOAD (MT) by LIU LiPing, HAN HaoHao, LIU JiaHuan, BAO Rui, LIN YueGuo

Subjects: “…Fuselage skin…”
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SIMULATION ANALYSIS OF CARGO LOADING ON CRASHWORTHINESS OF COMPOSITE FUSELAGE SECTION by XIE Jiang, MOU HaoLei, ZOU TianChun, FENG ZhenYu, MAO KeYi

Subjects: “…Composite fuselage section…”
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ANALYSIS AND EVALUATION FUSELAGE SECTION’S CRASHWORTHINESS OF TYPICAL CIVIL AIRPLANE BASED ON PASSENGER RESPONSE by ZHU XianFei, FENG YunWen, XUE XiaoFeng, ZHU ZhengZheng

Subjects: “…Fuselage section structure…”
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DAMAGE TOLERANCE EXPERIMENT AND ANALYSIS OF STIFFENED FUSELAGE PANEL WITH LONGITUDINAL CRACK by CHEN An, WEI YuLong, LIAO JiangHai, DONG DengKe

Subjects: “…Fuselage panel…”
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The crack path in fuselage panel under mixed mode biaxial loading by Alexander Zakharov, Valery Shlyannikov, Andrey Tumanov

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RESEARCH ON TEST METHOD OF FUSELAGE PANEL SUBJECTED TO SHEAR LOAD by ZANG WeiFeng, SU ShaoPu, ZHANG HaiYing, DONG DengKe

Subjects: “…Fuselage panel…”
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