High angle aerodynamic characteristics produced by nose cone of revolution in wind tunnel at supersonic speed


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg


    Contributors:

    Publication date :

    1960-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English