Theory of thin airfoils of small camber developed which permits either velocity distribution corresponding to given airfoil shape, or airfoil shape corresponding to given velocity distribution to be calculated; procedures to be employed are outlined and illustrated with suitable examples. (20¢) (released 1948)


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    Title :

    General theory of airfoil sections having arbitrary shape or pressure distribution


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Allen, H.J. (author)


    Publication date :

    1945


    Size :

    23 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :