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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    Titel :

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


    Weitere Titelangaben:

    Die Berechnung turbulenter, kompressibler Grenzschichten bei Einspritzung von Fremdgasen


    Beteiligte:
    Beddini, R.A. (Autor:in) / Sullivan, R.D. (Autor:in) / Fishburne, E.S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1976


    Format / Umfang :

    25 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




    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