Flow fields in two- and three-dimensional axisymmetric supersonic inlets are calculated with computer program that uses method of characteristics to compute array of points in flow field. At each point, local pressure, local Mach number, local flow angle, and static pressure are calculated. Program can be used to design and analyze supersonic inlets by determining surface compression rates and throat flow properties.


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    Titel :

    Flow fields in supersonic inlets


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1979-12-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Supersonic cruise inlets

    Bowditch, D. N. / Coltrin, R. E. / Sanders, B. W. et al. | NTRS | 1971


    Transient behavior of supersonic flow through inlets

    PORDAL, H. S. / KHOSLA, P. K. / RUBIN, S. G. | AIAA | 1992


    Transient behavior of supersonic flow through inlets

    Pordal, H. S. / Khosla, P. K. / Rubin, S. G. | NTRS | 1992


    Transient behavior of supersonic flow through inlets

    PORDAL, H. / KHOSLA, P. / RUBIN, S. | AIAA | 1990


    Flow field in supersonic mixed-compression inlets

    Bishop, A. R. / Hoffman, J. D. / Vadyak, J. | NTRS | 1980