Tests were made to determine effects of aileron contour modification on section aerodynamic characteristics of airfoil and aileron.
Two-dimensional wind-tunnel investigation of sealed 0.22-airfoil-chord internally balanced ailerons of different contour on NACA 65 (112)-213 airfoil
Nat Advisory Committee Aeronautics -- Tech Note
1946
16 pages
26 Supp sheets
Report
Englisch
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Engineering Index Backfile | 1945
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