Pressure distribution on trapezoidal wing of canard aircraft model in supersonic pressure tunnel - tables


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    Title :

    Tabulated data from a pressure-distribution investigation at Mach number 2.01 of the wing of a canard airplane model


    Contributors:
    Driver, C. (author) / Jacocks, J. L. (author)

    Publication date :

    1959-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English