Results from an investigation of the effects of the operation of a combined turbojet/scramjet propulsion system on the longitudinal aerodynamic characteristics of a 1/60-scale hypersonic airbreathing launch vehicle configuration are presented. Decomposition products of hydrogen peroxide were used for simulation of the propulsion system exhaust.


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    Titel :

    Investigation of Effect of Propulsion System Installation and Operation on Aerodynamics of an Airbreathing Hypersonic Airplane at Mach 0.3 to 1.2


    Beteiligte:
    J. M. Cubbage (Autor:in) / C. E. Mercer (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    94 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch