Abstract Multiparameter studies of the discharge coefficient dependence on the nozzle geometry and the presence of a condensed phase in combustion products were performed. The simulation results obtained satisfactorily agree with the well-known generalized data. The modern computational fluid dynamics methods were shown to be able to refine the generalized empirical relations.


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    Title :

    Simulation of a Rocket Engine Nozzle Discharge Coefficient


    Contributors:

    Published in:

    Russian Aeronautics ; 61 , 2 ; 257-264


    Publication date :

    2018-04-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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