Ailerons of 0.20 Airfoil Chord and True Contour with 0.35 Aileron-Chord Extreme Blunt Nose Balance on NACA 66,2-216 Airfoil, W. LETKO, H. G. DENACI and C. FREED; No. L-432 (Advance Confidential Report 3F18 June 1943) 14 p, 24 supp plates: Ailerons of 0.20 Airfoil Chord and True Contour with 0.60 Aileron-Chord Sealed Internal Balance on NACA 66,2-216 Airfoil, H. G. DENACI and J. D. BIRD; No. L-325 (Advance Confidential Report 3I14 Sept 1943) 12 p, 20 supp plates: Ailerons of 0.20 Airfoil Chord and True Contour With 0.35 Aileron-Chord Frise Balance on NACA 23012 Airfoil, W. LETKO and W. B. KEMP; No. L-433 (Advance Confidential Report 3H28 Aug 1943) 17 p, 29 supp plates: Ailerons of 0.20 Airfoil Chord and True Contour with 0.35 Aileron-Chord Extreme Blunt-Nose Balance on NA CA 23012 Airfoil, W. LETKO, T. A. HOLLINGWORTH and R. A. ANDERSON; No. L-434 (Advance Confidential Report 3K05 Nov 1943) 12 p, 37 supp plates: Pressure Distributions Over NACA 66,2-216 and NACA 23012 Ailfoils with Various Balances on 0.20-Chord Ailerons, W. LETKO and H. G. DENACI. (Advance Confidential Report 3F11 June 1943)


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    Title :

    Wind-tunnel tests of ailerons at various speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Reports



    Publication date :

    1943


    Size :

    13 pages


    Remarks:

    31 supp plate


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English