Nonsteady flow conditions in subsonic section of Laval nozzle to investigate nonlinear transverse combustion instability in liquid propellant rocket motors


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    A Theoretical Study of Nonlinear Transverse Combustion Instability in Liquid Propellant Rocket Motors


    Contributors:
    Zinn, B. T. (author)

    Publication date :

    1966-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English