The results of first year's efforts on a experimental base flow program are reported. The design and checkout for a Mach 3.0 axisymmetric wind tunnel with a model base diameter of 2.25 inches is described, as well as the automated data acquisition system. Experiments are reported on detailed static pressures for the diffuser wall, model wall and bases and near wake. Temperature measurements are presented to establish a near adiabatic wall condition. The relationship between the experimental program and propulsive external burning is discussed.


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    Title :

    Experiments and analysis related to external burning for propulsion


    Additional title:

    Experimente und Analysen mit und von aeusserer Verbrennung als Antriebsmittel


    Contributors:

    Published in:

    Publication date :

    1976


    Size :

    63 Seiten


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Experiments related external burning for propulsion

    Strahle, W.C. / Hubbartt, J.E. / Neale, D.H. et al. | Tema Archive | 1977


    External burning propulsion analysis

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