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    Title :

    Drag Measurements of a 34 Degree Swept-forward and Swept-back NACA 65-009 Airfoil of Aspect Ratio 2.7 as Determined by Flight Tests at Supersonic Speeds


    Contributors:

    Publication date :

    1947-02-20


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English