Effect of nose bluntness, fineness ratio, cone angle, and model base on aerodynamic characteristics of blunt bodies


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack up to 180 Deg


    Contributors:
    Babb, C. D. (author) / Fuller, D. E. (author) / Shaw, D. S. (author)

    Publication date :

    1963-05-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English