Supersonic rocket nozzle design for optimum thrust with chemically reacting gas flows


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Optimum thrust nozzle contours for chemically reacting gas flows


    Contributors:

    Publication date :

    1966-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English