Pressure distribution and pressure drag were determined on body which had jet issuing from nose at several free stream Mach numbers; as result of retrorocket operation large decrease in pressure drag occurred; at same time, retrorocket caused very unstable flow about model.


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    Titel :

    Investigation of retrorocket exhausting from nose of blunt body into supersonic free stream


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Charczenko, N. (Autor:in) / Hennessey, K.W. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :