Analytical method for ejector problem makes it possible to propose and exploit quantitatively entirely theoretical flow model for evaluating in-flight performance of vehicle-integrated air-augmented propulsion systems; using this flow model, ejector pumping characteristics, matching of ejector-intake system, gross thrust, and net thrust for in-flight performance evaluations of ejector nozzles can be determined theoretically; theory is capable of predicting cold and hot flow operating characteristics as well as influence of different values of specific heat ratios.


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    Titel :

    Installed performance of air-augmented nozzles based on analytical determination of internal ejector characteristics


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Korst, H.H. (Autor:in) / Addy, A.L. (Autor:in) / Chow, W.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch