Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 651-210 airfoil section
Wartime report ; L-151
1945
19 S.
Ill., graph. Darst.
Originally issued December 1945 as Advance confidential report L5F27
Report
Englisch
Engineering Index Backfile | 1945
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