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    Title :

    Optimal weight of cracked composite panels by an equivalent strain constraint


    Contributors:

    Conference:

    19th AIAA Applied Aerodynamics Conference ; 2001 ; Anaheim , CA , U.S.A.



    Publication date :

    2001-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    RESPONSE SURFACES FOR OPTIMAL WEIGHT OF CRACKED COMPOSITE PANELS: NOISE AND ACCURACY

    Papila, M. / Haftka, R. T. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2000




    Residual Strength of Cracked Stiffened Panels

    D. Broek / H. Vlieger | NTIS | 1967


    Computation of energy release rates for cracked composite panels with nonlinear deformation

    Wang, John / Xue, David / Sleight, David et al. | AIAA | 1995