Pressure distribution over thin airfoil of infinite span is calculated by integrating disturbances due to appropriate distribution of sources over forepart of Mach cone for point at which pressure is desired; result expressed in terms of Green's function giving pressure at any point on airfoil due to unit harmonic velocity at any other point. (correction) n 11 Nov p 630.


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    Title :

    Aerodynamic forces on oscillating airfoil at supersonic speeds


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Miles, J.W. (author)


    Publication date :

    1947


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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