Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 652-415, 653-418 and 654-421 airfoil sections. (Confidential Bul L4H12 Aug 1944)
Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 652-415, 653-418 and 654-421 airfoil sections
Nat Advisory Committee Aeronautics -- Wartime Report
1944
9 pages
8 supp plates
Report
English
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