Program computes compressible laminar boundary-layer flow over yawed infinite wing including distributed suction. Computations are useful in efforts to implement boundary-layer suction on wing to maintain laminar flow in order to reduce net drag. Program contains number of approximations to simplify analysis; yet results are accurate enough to be useful, particularly in preliminary design phase.


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    Title :

    Compressible laminar boundary-layer flow


    Contributors:

    Published in:

    Publication date :

    1978-03-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :