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 : Subsonic Mach and Reynolds Number Effects on the Characteristics of the Wing and on the Effectiveness of an Elevon


    Contributors:

    Publication date :

    1948-10-11


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English