Derivation of point source method based on linearized theory for obtaining pressure coefficient on thin wings at supersonic speeds.


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    Title :

    Theoretical distribution of lift on thin wings at supersonic speeds (extension)


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    49 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :