Existing steady-state 3-D computer program for calculating gasturbine flow fields modified to include computation of soot and nitrogen oxide emission. In addition, radiation calculation corrected for soot particles. These advanced tools offer potential of reducing design and development time required for gas-turbine combustors.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Computation of Three-Dimensional Combustor Performance


    Beteiligte:
    Srivatsa, S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1985-01-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Three dimensional hot flow computation of the aero gas turbine combustor

    Sivaramakrishna, G. / Muthuveerappan, N. / Shankar, V. et al. | British Library Conference Proceedings | 2000



    Computations of three-dimensional gas turbine combustor flows

    MOSTAFA, A. / MENDILLO, J. / MARCHIONNA, N. | AIAA | 1991



    Computation of losses in a scramjet combustor

    KAMATH, PRADEEP / MCCLINTON, CHARLES | AIAA | 1992