Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 652-415, 653-418 and 654-421 airfoil sections. (Confidential Bul L4H12 Aug 1944)


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    Title :

    Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 652-415, 653-418 and 654-421 airfoil sections


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1944


    Size :

    9 pages


    Remarks:

    8 supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English