Analytical method for including thermodynamic data with variable isentropic exponent in method of characteristics as applied to design of high-temperature rocket exhaust nozzles is obtained; several bell-shaped nozzles are designed and nozzle contours compared showing that significant differences occur; conclusions presented.


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    Titel :

    Design of axisymmetric exhaust nozzles by method of characteristics incorporating variable isentropic exponent


    Weitere Titelangaben:

    NASA -- Tech Report


    Beteiligte:
    Guentert, E.C. (Autor:in) / Neumann, H.E. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch