Convergent solution for clamped parallelogrammic panels subjected to uniform lateral pressure is found by means of power series and Galerkin's technique; results for center deflections and maximum moments at center and along edges are presented; tests are carried out on four aluminum-alloy panels to substantiate and verify theory; applicability to aircraft wings.


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    Title :

    Theoretical and experimental investigations of thin parallelogrammic panels


    Additional title:

    Can Aeronautics Space J


    Contributors:


    Publication date :

    1967


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :