The Solid Rocket Motor Air Flow Equipment (SRMAFTE) facility was constructed for the purpose of evaluating the internal propellant, insulation, and nozzle configurations of solid propellant rocket motor designs. This makes the characterization of the facility internal flow field very important in assuring that no facility induced flow field features exist which would corrupt the model related measurements. In order to verify the design and operation of the facility, a three-dimensional computational flow field analysis was performed on the facility checkout model setup. The checkout model measurement data, one-dimensional and three-dimensional estimates were compared, and the design and proper operation of the facility was verified. The proper operation of the metering nozzles, adapter chamber transition, model nozzle, and diffuser were verified. The one-dimensional and three-dimensional flow field estimates along with the available measurement data are compared.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    SRMAFTE facility checkout model flow field analysis


    Beteiligte:


    Erscheinungsdatum :

    01.07.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Injector/Chamber Scaling Evaluation, Facility Checkout

    M. F. Powell / P. W. Powell / M. J. Fleiszar et al. | NTIS | 1969


    METHOD OF FACILITY CHECKOUT OF AUTOMATIC CAB SIGNALLING

    BATRAEV VLADIMIR PETROVICH / MARSHOV SERGEJ VLADIMIROVICH | Europäisches Patentamt | 2018

    Freier Zugriff

    AUTOMATED CHECKOUT

    HUMPHRYS DOUGLAS E | Europäisches Patentamt | 2018

    Freier Zugriff

    CHECKOUT SYSTEM

    GOTANDA TSUYOSHI | Europäisches Patentamt | 2017

    Freier Zugriff

    EXPEDITED CHECKOUT SYSTEM THROUGH PORTABLE CHECKOUT UNITS

    CHAUBARD FRANCOIS / GARAFULIC ADRIANO QUIROGA | Europäisches Patentamt | 2017

    Freier Zugriff