The buckling analysis presented considers rectangular flat or curved general laminates subjected to combined inplane normal and shear loads. Linear theory is used in the analysis. All prebuckling deformations and any initial imperfections are ignored. The analysis method can be readily extended to longitudinally stiffened structures subjected to combined inplane normal and shear loads.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Buckling analysis for anisotropic laminated plates under combined inplane loads


    Contributors:

    Conference:

    International Astronautical Federation, International Astronautical Congress ; 1974 ; Amsterdam, Netherlands


    Publication date :

    1974-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English