Results and discussion of lateral control investigation; data obtained through large angle-of-attack range and at Mach numbers from 0.13 to 0.71.


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    Title :

    High-speed wind-tunnel investigation of NACA 65-210 semispan wing equipped with plug and retractable ailerons and full-span slotted flap


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    81 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English