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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    Title :

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


    Additional title:

    NASA -- Tech Report


    Contributors:


    Publication date :

    1959


    Size :

    31 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English