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    Title :

    Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel IV : the Effect of a Constant-chord Leading-edge Flap at High Subsonic Speeds


    Contributors:

    Publication date :

    1949-01-20


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English