The up-to-date methods of computational fluid dynamics (CFD) were employed to study the effect of mass flux ratio above the submerged part of a solid rocket engine nozzle with a contoured inlet on the discharge coefficient. The results are given in correlation with the inlet geometry and nozzle submergence.


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    Title :

    Effect of Mass Flux Ratio above the Submerged Part of a Nozzle with a Contoured Inlet on the Discharge Coefficient


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 63 , 2 ; 310-316


    Publication date :

    2020-04-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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