Turbulent base flowfields in multinozzle configurations, considering adiabatic flow and determining base pressure distribution from reverse jet impingement


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    A theory for base pressures on multinozzle rocket configurations


    Contributors:
    Abbud, K. A. (author) / Lamb, J. P. (author) / Lenzo, C. S. (author)

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 5TH, U.S. AIR FORCE ACADEMY ; 1969 ; COLORADO SPRINGS, CO


    Publication date :

    1970-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    A theory for base pressures on multinozzle rocket configurations

    ABBUD, K. A. / LAMB, J. P. / LENZO, C. S. | AIAA | 1970


    A theory for base pressures on multinozzle rocket configurations

    ABBUD, K. / LAMB, J. / LENZO, C. | AIAA | 1969


    Base Thermal Environment on Multinozzle Rocket Configurations

    Wang, Xu / Xu, Xu / Yang, Qingchun | AIAA | 2022


    A theory for base pressures in multi-nozzle rocket configurations.

    Abbud, K. A. / Lamb, J. P. / Lenzo, C. S. | NTRS | 1969