PREDICTION AND DAMAGE ANALYSIS OF THE POSTBUCKLING FOR MULTI-SPAR COMPOSITE BOX by YUAN Fei, CHAI YaNan, ZHANG AYing

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DAMAGE EXPANSION OF STIFFENED PANEL WITH PREFABRICATED DEBONDING by ZHANG Ru, CHAI YaNan, ZHANG Aying, CHEN XiangMing

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LOAD TRANSFER ANALYSIS IN BONDED-BOLTED HYBRID JOINTS by CHEN XiangMing, CHAI YaNan, YUAN Fei, YU Fei, CAO Su

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STIFFENER-SKIN INTERFACE FAILURE CHARACTERIZATION OF THE STIFFENED COMPOSITE PANEL AT POST-BUCKLING STAGE by HU BoTao, CHAI YaNan, CHEN XiangMing, WEI JingChao

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INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT) by YUAN Fei, LIU Fu, CHAI YaNan, CHEN XiangMing, LIN GuoWei, LI XinXiang

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INVESTIGATION OF REPAIR TECHNIQUE FOR AIRCRAFT COMPOSITE WING PANEL WITH DISCRETE-SOURCE DAMAGE by CHEN XiangMing, ZHANG AYing, CHAI YaNan, LIU HongWu, WANG LiLi, YU Fei

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ASSESSMENT METHOD OF THE REPAIRED AIRCRAFT COMPOSITE WING PANEL WITH DISCRETE-SOURCE DAMAGE by CHEN XiangMing, ZHANG AYing, CHAI YaNan, LIU HongWu, WANG LiLi, YU Fei

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