Wind-tunnel tests of ailerons at various speeds 2: ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil

Author: Denaci, H. G.
Year: 1943
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-432, NACA-ACR-3F18
Link: https://digital.library.unt.edu/ark:/67531/metadc61625/

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