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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Hypervelocity scramjet combustor-nozzle analysis and design


    Contributors:

    Publication date :

    1992-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Hypervelocity Scramjet Combustor-Nozzle Analysis and Design

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


    Scramjet combustor and nozzle computations

    Kamath, Pradeep S. / Mcclinton, Charles R. | NTRS | 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