Composite-Plate-Buckling Analysis Program (COMPPAP) helps engineers determine buckling loads of orthotropic or isotropic irregularly shaped plates without need to perform manual calculations and extensive finite-element mathematical modeling. One-element finite-element program utilizing high-order displacement functions to perform plane-stress analysis of general plate followed by buckling calculation based on stresses found in plane-stress solution. High order of displacement functions enables user to obtain results more accurately. Written in ANSI FORTRAN 77. Two machine versions available: (MSC-22428) for computers of IBM PC 386 and higher series and for compatible computers; and UNIX (MSC-22286).


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    Titel :

    Composite-Plate-Buckling Analysis Program


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1994-12-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Viscoelastic analysis of laminated plate buckling

    WILSON, D. W. / VINSON, J. R. | AIAA | 1984


    Buckling analysis of ship plate-structures1

    Geertsema, H. | IOS Press | 1977


    Reliability analysis and reliability-based design of composite laminated plate subject to buckling

    Kogiso, Nozomu / Shao, Shaowen / Murotsu, Yoshisada et al. | AIAA | 1997