Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Optimal sizing of a composite sandwich fuselage component


    Contributors:


    Publication date :

    2001



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    Local classification TIB:    275/4530/7025
    BKL:    55.20 / 55.20 Straßenfahrzeugtechnik



    Optimal sizing of a composite sandwich fuselage component

    Ley,R. / Peltier,A. / Northrop Grumman,US | Automotive engineering | 2001


    Optimal sizing of a composite sandwich fuselage component

    Ley, R. / Peltier, A. | Tema Archive | 2001


    STRINGERLESS SANDWICH FUSELAGE PANELS

    SONG WEIDONG | European Patent Office | 2020

    Free access

    STRINGERLESS SANDWICH FUSELAGE PANELS

    SONG WEIDONG | European Patent Office | 2024

    Free access

    Stringerless sandwich fuselage panels

    SONG WEIDONG | European Patent Office | 2020

    Free access