Effects of conical camber for triangular wing- body-tail combinations on aerodynamic characteristics


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    Title :

    A Wind-Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration Having a Triangular Wing of Aspect Ratio 2.2


    Contributors:
    Boyd, J. W. (author) / Phelps, E. R. (author)

    Publication date :

    1957-04-30


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English