Perforated wall nozzle providing variable Mach number supersonic flow for external stream simulation in rocket propulsion tests


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    Title :

    A new concept of a variable-Mach-number perforated wall nozzle for providing a supersonic external stream in rocket-propulsion testing.


    Contributors:

    Conference:

    FLIGHT TEST, SIMULATION AND SUPPORT CONFERENCE ; 1968 ; LOS ANGELES, CA


    Publication date :

    1968-03-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English