A second-order closure technique for the compressible turbulent boundary layer equations has been developed. The technique is employed in the calculation of boundary layers with surface injection of similar and foreign gases. Theoretical results for M approximately 3 and several air injection rates provide favorable comparison with experimental data. Theoretical mean velocity and mass fraction profiles for a propane injected oxygen boundary layer are also presented.


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    Title :

    The calculation of turbulent compressible boundary layers with injection of a foreign gas


    Additional title:

    Die Berechnung turbulenter, kompressibler Grenzschichten bei Einspritzung von Fremdgasen


    Contributors:

    Published in:

    Publication date :

    1976


    Size :

    25 Seiten


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Compressible turbulent boundary layers with injection

    SQUIRE, L. C. / THOMAS, G. D. / MARRIOTT, P. G. | AIAA | 1977





    SYNOPTIC: Calculation of Compressible Adiabatic Turbulent Boundary Layers

    TUNCER CABECI / A.M.O. SMITH / AND G. MOSINSKIS | AIAA | 1970