Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on NACA 651-210 airfoil section. (Confidential Report L5F27 Dec 1945)
Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on NACA 651-210 airfoil section
Nat Advisory Committee Aeronautics -- Wartime Report
1945
19 pages
37 Supp plates
Report
English
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