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    Title :

    Buckling Load Reduction for Stiffened Panels Due to Cutouts in Ribs



    Published in:

    Publication date :

    1998



    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



    Buckling Load Reduction for Stiffened Panels Due to Cutouts in Ribs

    A. Watson / F. Williams / D. Kennedy | AIAA | 1998


    Buckling load reduction for stiffened panels due to cutouts in ribs

    Watson, A. / Williams, F.W. / Kennedy, D. | Tema Archive | 1998


    Thermomechanical buckling of multilayered composite panels with cutouts

    Noor, Ahmed K. / Starnes, James H. / Peters, Jeanne M. | AIAA | 1994


    Ultimate Strength of Stiffened Panels with Cutouts under Uniaxial Compression

    Alagusundaramoorthy, P. / Sundaravadivelu, R. / Ganapathy, C. | British Library Online Contents | 1995


    Thermomechanical buckling of multilayered composite panels with cutouts

    Noor, Ahmed K. / Starnes, James H., Jr. / Peters, Jeanne M. | NTRS | 1994