The progress report for the grant entitled 'Hypervelocity of Scramjet Combustor-Nozzle Analysis and Design' is presented. The three main tasks in the program are combustor modeling study, development of anaylsis capabilities for hypersonic scramjet nozzles, and development of optimum design methods for hypersonic scramjet nozzles. The research performed was documented in a series of technical publications and presentations at various conferences. A brief description of the research in each of the above three areas and a list of the resulting technical publications are included.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hypervelocity scramjet combustor-nozzle analysis and design


    Beteiligte:

    Erscheinungsdatum :

    1992-11-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hypervelocity Scramjet Combustor-Nozzle Analysis and Design

    H. D. Thompson / J. D. Hoffman | NTIS | 1992


    Scramjet Combustor and Nozzle Computations

    Kamath, P. S. / McClinton, C. R. | British Library Online Contents | 1992


    Numerical Study of Hypervelocity Flows Through a Scramjet Combustor

    R. Krishnamurthy / R. C. Rogers / S. N. Tiwari | AIAA | 1997



    A Numerical Study of Hypervelocity Flows Through a Scramjet Combustor

    Krishnamurthy, R. / Rogers, R. C. / Tiwari, S. N. et al. | British Library Conference Proceedings | 1994