Abstract The problem of determining the “potential” number of integration steps by explicit difference schemes is solved within the framework of the prediction model for chemically non-equilibrium processes.


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    Title :

    Difference schemes in computations for chemically non-equilibrium processes in the rocket engine nozzles


    Contributors:

    Published in:

    Russian Aeronautics ; 60 , 1 ; 103-109


    Publication date :

    2017-01-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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