A JANNAF sponsored workshop was held to discuss the importance and role of radiative heat transfer in rocket combustion chambers. The potential impact of radiative transfer on hardware design, reliability, and performance was discussed. The current state of radiative transfer prediction capability in CFD modeling was reviewed and concluded to be substantially lacking in both the physical models used and the radiative property data available. There is a clear need to begin to establish a data base for making radiation calculations in rocket combustion chambers. A natural starting point for this effort would be the NASA thermochemical equilibrium code (CEC).


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Radiation Effects on Flow Characteristics in Combustion Chambers


    Contributors:

    Publication date :

    1989


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Combustion interaction with radiation-cooled chambers

    ROSENBERG, S. / JASSOWSKI, D. / BARLOW, R. et al. | AIAA | 1990


    A numerical study of radiation effects in gas turbine combustion chambers

    Eklund, Dean / Badinand, Thomas / Fransson, Torsten | AIAA | 1998



    Heat transfer characteristics of H2/O2-combustion chambers

    FROEHLICH, A. / POPP, M. / SCHMIDT, G. et al. | AIAA | 1993


    Experiments on the Flow Characteristics Behind Swirl Nozzles in Atmospheric Combustion Chambers

    Lehmann, B. / Mante, J. / International Society for Air Breathing Engines | British Library Conference Proceedings | 1999