Asymptotic solutions are obtained for unsteady pressure on wings and bodies that oscillate harmonically while in supersonic flight; solutions have form of series in descending powers of frequency, and include effects of 3-dimensional flow and second-order effects due to thickness of wing; results consist of first 2 terms of series for 3-dimensional wings with supersonic trailing edges, first 3 terms of series for supersonic 2-dimensional airfoils, and first 4 terms for very slender wings and bodies.


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    Title :

    Aerodynamics of supersonic wings and bodies oscillating at high frequency


    Additional title:

    Haifa, Israel Inst Technology -- Dept Aeronautical Eng -- Report


    Contributors:
    Hanin, M. (author)


    Publication date :

    1963


    Size :

    42 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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