Wind Tunnel Tests of Ailerons at Various Speeds 1: Ailerons of 0.20 Airfoil Chord and True Contour With 0.35 Aileron-Chord Extreme Blunt Nose Balance on the NACA 66,2-216 Airfoil

Author: Letko, W.
Additional Authors: Denaci, H. G.
Year: 1943
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-431, NACA-ACR-3F11
Link: https://digital.library.unt.edu/ark:/67531/metadc61624/

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