In addition to fixed and variable bleed devices provided for controlling the position of a terminal shock wave in a supersonic inlet, a plurality of free piston valves are disposed around the periphery of a cowling of a supersonic engine inlet. The free piston valves are disposed in dump passageways, each of which begin at a bleed port in the cowling that is located in the throat region of the inlet, where the diameter of the centerbody is near maximum, and terminates at an opening in the cowling adjacent a free piston valve. Each valve is controlled by reference pressure.


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    Titel :

    Airflow Control System for Supersonic Inlets


    Beteiligte:
    G. A. Mitchell (Autor:in) / B. W. Sanders (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Airflow control system for supersonic inlets

    Mitchell, G. A. / Sanders, B. W. | NTRS | 1974


    AIRFLOW CONTROL SYSTEM FOR SUPERSONIC INLETS

    G. A. Mitchell / B. W. Sanders | NTIS | 1971


    Supersonic cruise inlets

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


    Inlets for supersonic missiles

    Mahoney, John J. | TIBKAT | 1990


    Flow fields in supersonic inlets

    Sorensen, V. L. | NTRS | 1979