Wind-tunnel investigation of blunt-nose aileron with beveled trailing edge on NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour. (Advance Confidential Report L5B10 Feb 1945)
Wind-tunnel investigation of blunt-nose aileron with beveled trailing edge on NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour
Nat Advisory Committee Aeronautics -- Wartime Report
1945
13 pages
23 supp plates
Report
Englisch
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