Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90-degrees


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    EFFECT OF LONGITUDINAL AND LATERAL CONTROLS ON AERODYNAMIC CHARACTERISTICS OF A WINGED REENTRY CONFIGURATION AT A MACH NUMBER OF 1.97 AND ANGLES OF ATTACK UP TO APPROXIMATELY 90 DEG


    Contributors:

    Publication date :

    1961-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English