In this report a theory of thin airfoils of small camber is developed which permits either the velocity distribution corresponding to a given airfoil shape, or the airfoil shape corresponding to a given velocity distribution to be calculated. The procedures to be employed in these calculations are outlined and illustrated with suitable examples.


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    Title :

    General theory of airfoil sections having arbitrary shape or pressure distribution


    Contributors:

    Publication date :

    1945-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English