An analysis of turbulent convective and radiative heat fluxes in high temperature environments is presented. A second-order turbulence closure model along with a differential approximation for the calculation of radiative heat flux are incorporated into the numerical solution of a high temperature flowfield (created by a specified energy addition), to simulate the environment of advanced rocket chamber flows.


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    Title :

    Analysis of turbulent convective and radiative heat transfer in high temperature rocket chamber flows


    Additional title:

    Analyse von turbulentem konvektivem und radiativem Waermeuebergang in Hochtemperaturraketenkammerstroemungen


    Contributors:
    Beddini, R.A. (author) / Owano, T.G. (author)

    Published in:

    AIAA-Papers ; Jul ; 1-6


    Publication date :

    1987


    Size :

    6 Seiten, 7 Bilder, 14 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English