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    Titel :

    A Semi-Analytical Approach for Predicting the Post-Buckling Response of Laminates with a Cutout


    Beteiligte:
    Barut, Atila (Autor:in) / Madenci, Erdogan (Autor:in)

    Kongress:

    47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference



    Erscheinungsdatum :

    01.01.2006




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    AIAA-2006-1786 A Semi-Analytical Approach for Predicting the Postbuckling Response of Laminates with a Cutout

    Barut, A. / Madenci, E. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006



    AIAA-2006-1785 Buckling Analysis of Laminates with a Cutout Using a Zeroth-Order Shear Deformation Theory

    Barut, A. / Madenci, E. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006


    Damage progression in compressively loaded laminates containing a circular cutout

    Waas, A.M. / Babcock, C.D. jun. / Knauss, W.G. | Tema Archiv | 1991


    Damage progression in compressively loaded laminates containing a circular cutout

    WAAS, A. M. / KNAUSS, W. G. / BABCOCK, C. D. | AIAA | 1991