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    Title :

    Wind-Tunnel Tests of Ailerons at Various Speeds. 3 - Ailerons of 0.20 Airfoil Chord and True Contour with 0.35-Aileron-Chord Frise Balance on the NACA 23012 Airfoil


    Contributors:
    W. Letko (author) / W. B. Kemp (author)

    Publication date :

    1943


    Size :

    35 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English