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    Title :

    High-Speed Wind-Tunnel Tests of an NACA 16-009 Airfoil Having a 32.9- Percent-Chord Flap with an Overhang 20.7 Percent of the Flap Chord


    Contributors:

    Publication date :

    1947


    Size :

    40 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English