Wind Tunnel Tests of Ailerons at Various Speeds 4: Ailerons of 0.20 Airfoil Chord and True Contour With 0.35 Aileron-Chord Extreme Blunt-Nose Balance on the NACA 23012 Airfoil

Author: Anderson, R. A.
Year: 1943
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-433, NACA-ACR-3H28
Link: https://digital.library.unt.edu/ark:/67531/metadc61629/

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