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

Author: Letko, W.
Year: 1943
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-325, NACA-ACR-3I14
Link: https://digital.library.unt.edu/ark:/67531/metadc61626/

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