Use of effective width of sheet acting with stiffener has found favor with designers, and paper is primarily concerned with methods of calculating effective width, not only at ultimate strength of panel, but also at lower loads.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Stress distribution in stiffened panels under compression


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Sechler, E.E. (Autor:in)


    Erscheinungsdatum :

    1937


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Stiffened Carbon/Carbon Compression Panels

    Sawyer, James W. | NTRS | 1992


    Weight-Effect of Buckled Composite Stiffened Panels Under Static Compression

    Goyal, Vijay / Gagliano, Jacob N. / Pennington, Austin et al. | AIAA | 2023


    Ultimate Strength of Stiffened Panels with Cutouts under Uniaxial Compression

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