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    Title :

    Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps - Trailing-edge Flaps Deflected


    Contributors:

    Publication date :

    1950-12-13


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English