Characteristics of plug nozzle are compared with converging diverging nozzle; mathematical analysis of aerodynamic performance of plug nozzle including Prandtl-Meyer corner expansion of flowing gas; advantages of plug nozzle in terms of superior performance at lower than design pressure ratio, smaller physical size and aerodynamic thrust vector control and how they can be utilized in liquid propellant rockets.


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    Title :

    Performance of plug-type rocket exhaust nozzles


    Additional title:

    ARS J


    Contributors:

    Published in:

    ARS Journal ; 31 , n 1


    Publication date :

    1961


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :