The paper presents a physical-mathematical and computational model of the flow in a rocket engine nozzle. The combustion products of the fuel are simulated as a mixture of perfect gases, taking into account the dependence of the thermodynamic properties of the components on the temperature and pressure. To simulate the chemical equilibrium and nonequilibrium flows, a direct problem of the nozzle theory is solved. The results of comparison between the calculated and the reference data are provided.


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    Titel :

    One-Dimensional Model for Calculating Losses due to Chemical Nonequilibrium in a Rocket Engine Nozzle


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:

    Erschienen in:

    Russian Aeronautics ; 67 , 3 ; 601-609


    Erscheinungsdatum :

    01.09.2024


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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    Rocket engine nozzle photographic system

    Bailey, R. L. / Tibbitts, W. C. | NTRS | 1968