Method for determining streamline flow pattern of nonviscous incompressible fluid about oblique airfoil from corresponding flow pattern about airfoil in normal position is presented and illustrated with two examples; method can be extended to account approximately for compressibility effects by applying Prandtl-Glauert correction factor to flow pattern that is normal to leading edge of airfoil.


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    Title :

    Streamline pattern in vicinity of oblique airfoil


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    7 pages


    Remarks:

    20 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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