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    Title :

    Low-subsonic Investigation to Determine the Chordwise Pressure Distribution and Effectiveness of Spoilers on a Thin, Low-aspect-ratio, Unswept, Untapered, Semispan Wing and on the Wing with Leading- and Trailing-edge Flaps


    Contributors:

    Publication date :

    1958-04-23


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English