Hasil Pencarian - CHAI YaNan

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  1. 1
    PREDICTION AND DAMAGE ANALYSIS OF THE POSTBUCKLING FOR MULTI-SPAR COMPOSITE BOX

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

    Diterbitkan 2018-01-01
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  2. 2
    DAMAGE EXPANSION OF STIFFENED PANEL WITH PREFABRICATED DEBONDING

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

    Diterbitkan 2020-01-01
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  3. 3
    LOAD TRANSFER ANALYSIS IN BONDED-BOLTED HYBRID JOINTS

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

    Diterbitkan 2017-01-01
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  4. 4
    STIFFENER-SKIN INTERFACE FAILURE CHARACTERIZATION OF THE STIFFENED COMPOSITE PANEL AT POST-BUCKLING STAGE

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

    Diterbitkan 2019-01-01
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  5. 5
    INTERNAL CLADDING LAYER INFLUENCE ON THE DEBONDING OF HAT-STRINGER STIFFENED COMPOSITE PANELS UNDER AXIAL COMPRESSION (MT)

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

    Diterbitkan 2022-01-01
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  6. 6
    INVESTIGATION OF REPAIR TECHNIQUE FOR AIRCRAFT COMPOSITE WING PANEL WITH DISCRETE-SOURCE DAMAGE

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

    Diterbitkan 2017-01-01
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  7. 7
    ASSESSMENT METHOD OF THE REPAIRED AIRCRAFT COMPOSITE WING PANEL WITH DISCRETE-SOURCE DAMAGE

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

    Diterbitkan 2017-01-01
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