Analysis of hypersonic ramjet cycles shows that supersonic combustion is requirement; paper presents experimental results where supersonic combustion in constant area duct is initiated by shock wave, evaluates possibility of analyzing data with one-dimensional flow equations, determines how closely current chemical kinetic computations agree with experimental results, and discusses problems encountered; shock-induced combustion is experimentally feasible in ducted flow, and can be controlled by varying inlet temperature, pressure, Mach number, on fuel concentration.


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    Titel :

    Shock-induced supersonic combustion in constant-area duct


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Rubins, P.M. (Autor:in) / Cunningham, T.H.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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