A potential flow routine and a viscous boundary layer routine have been combined into a single routine for estimating the flow in and around subsonic inlets. In this combined routine, the viscous flow solution about the inlet body is obtained by adding the viscous displacement thickness to the inlet geometry. Combination of the two flow solutions has resulted in cost savings, both in preparation time and in computer time. This routine is a useful tool in optimizing lip shapes for V/STOL inlets. The method of combining the routine, comparison with NASA test data, and utilization of the routine for V/STOL inlet design are presented.(Buehn)


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    Titel :

    A combined potential and viscous flow solution for V/STOL engine inlets


    Weitere Titelangaben:

    Ein kombiniertes Rechnerprogramm fuer Potential- und zaehe Stroemung zur Auslegung von Kurzstarttriebwerkseinlaeufen


    Beteiligte:
    Ybarra, A.H. (Autor:in) / Rhoades, W. (Autor:in) / Stockman, N.O. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1978


    Format / Umfang :

    7 Seiten, 11 Bilder, 1 Tabelle, 5 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    A combined potential and viscous flow solution for V/STOL engine inlets

    YBARRA, A. / RHOADES, W. / STOCKMAN, N. | AIAA | 1978



    Prediction of Boundary-Layer Flow Separation in V/STOL Engine Inlets

    D.C. Chou / R.W. Luidens / N.O. Stockman | AIAA | 1978



    Zero-length inlets for subsonic V/STOL aircraft

    GLASGOW, E. R. / BECK, W. E. / WOOLLETT, R. R. | AIAA | 1983