Simple approximate method given for calculation of isentropic irrotational flows past symmetrical airfoils, including mixed subsonic-supersonic flows; method based on choice of suitable values for streamline curvature in flow field and subsequent integration of equations of motion.


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    Title :

    Calculation of compressible flows past aerodynamic shapes by use of streamline curvature


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Perl, W. (author)


    Publication date :

    1947


    Size :

    38 pages


    Remarks:

    49 Supp Plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :