Linearized solution for oscillating 3-dimensional airfoil is extended to include higher order terms in angle of attack and thickness so that relative importance of, tendencies indicated by, second order terms may be evaluated.


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    Title :

    Second-order solution for oscillating two-dimensional supersonic airfoil


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Wylly, A. (author)

    Published in:

    Publication date :

    1952


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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