As flight speeds increase, supersonic aircraft powerplant installations may encounter complex aerodynamic problems due to shock reflection and possibility of inlet shock instability created by pod-to-pod interference; experimental program conducted at United Aircraft Corp and wind tunnel test data obtained during study of adjacent inlet interference are presented; program established, for Mach 3.0 design mixed compression inlet, dividing line between regions of expelled shock interference and completely stable operation; study was also conducted to determine effect of placing plate between pods.


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    Titel :

    Inlet-to-inlet shock interference tests


    Weitere Titelangaben:

    NASA CR


    Beteiligte:
    Motycka, D.L. (Autor:in) / Murphy, J.B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    45 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




    Inlet-to-inlet shock interference tests

    Motycka, D. L. / Murphy, J. B. | TIBKAT | 1965


    Inlet-to-inlet shock interference tests final report

    Motycka, D. L. / Murphy, J. B. | NTRS | 1965


    Inlet-TO-Inlet Shock Interference Tests Final Report

    D. L. Motycka / J. B. Murphy | NTIS | 1965


    Experimental investigation of inlet-to-inlet shock interference

    Motycka, D.L. / Murphy, J.B. | Engineering Index Backfile | 1965


    Experimental Investigation of Inlet-to-Inlet Shock Interference

    Motycka, D. L. / Murphy, J. B. | SAE Technical Papers | 1965