Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    STRUCTURAL MECHANICS AND MATERIALS - Prediction of Residual Strength and Curvilinear Crack Growth in Aircraft Fuselages



    Published in:

    Publication date :

    2002



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.93 / 55.50 Luftfahrzeugtechnik / 50.93 Weltraumforschung / 55.60 Raumfahrttechnik / 55.50 / 55.60
    Local classification TIB:    770/7040



    Prediction of Residual Strength and Curvilinear Crack Growth in Aircraft Fuselages

    Chuin-Shan Chen / Paul A. Wawrzynek / Anthony R. Ingraffea | AIAA | 2002


    Prediction of residual strength and curvilinear crack growth in aircraft fuselages

    Chen, C.S. / Wawrzynek, P.A. / Ingraffea, A.R. | Tema Archive | 2002



    Residual strength prediction of aircraft fuselages using crack-tip opening angle criterion

    Chen, C.S. / Wawrzynek, P.A. / Ingraffea, A.R. | Tema Archive | 2002


    Residual Strength Prediction of Aircraft Fuselages Using Crack-Tip Opening Angle Criterion

    Chuin-Shan Chen / Paul A. Wawrzynek / Anthony R. Ingraffea | AIAA | 2002