Automatic, minimum weight optimum design capability for rectangular, simply supported waffle plates subjected to multiplicity of inplane load conditions is presented; synthesis involves 6 design parameters which are given; mathematical programming problem to which synthesis leads has following characteristics -- relative minima, nonlinear inequality constraints, multitude of side constraints, and nonlinear merit function; numerical results for symmetric and unsymmetrical waffle-plate optimum designs are presented; applicability to space vehicle design.


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    Title :

    Structural synthesis capability for integrally stiffened waffle plates


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 1 , n 12


    Publication date :

    1963


    Size :

    17 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Structural synthesis capability for integrally stiffened waffle plates

    Kicher, T. P. / Morrow, W. M. / Schmit, L. A., Jr. | NTRS | 1964


    Structural synthesis capability for integrally stiffened waffle plates

    KICHER, T. P. / MORROW, W. M. / SCHMIT, L. A. | AIAA | 1963


    Structural synthesis capability for integrally stiffened waffle plates

    SCHMIT, JR., L. / KICHER, T. / MORROW, W. | AIAA | 1963


    A REPORT ON A STRUCTURAL SYNTHESIS CAPABILITY FOR INTEGRALLY STIFFENED WAFFLE PLATES

    Kicher, T. P. / Morrow, W. M. / Schmit, L. A., Jr. | NTRS | 1963


    A REPORT ON A STRUCTURAL SYNTHESIS CAPABILITY FOR INTEGRALLY STIFFENED WAFFLE PLATES

    Kicher, T. P. / Morrow, W. M., II / Schmit, J. A., Jr. | NTRS | 1963