Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic Characteristics at Mach Numbers from 0.7 to 1.75 of a Four-engine Swept-wing Airplane Configuration as Obtained from a Rocket-propelled Model Test


    Contributors:

    Publication date :

    1955-09-02


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English