Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effect of Sideslip on Aerodynamic Characteristics at a Mach Number of 1.4 with the Wing Twisted and Cambered


    Contributors:

    Publication date :

    1950-09-29


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English