Free-Spinning Wind-Tunnel Tests of a Low-Wing Monoplane with Systematic Changes in Wings and Tails IV : Effect of Center-of-Gravity Location (1939)
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FREE-SPINNING WIND-TUNNEL TESTS OF A LOW-WING MONOPLANE … (b) (a) (1) Rectangular wing with Army tips; (2) rectangular wing with interchange- (a) Front view. able rectangular and faired tips; (3) 5:2 tapered wing with Army tips; (4) 2:1 Army (b) Plan view. standard tapered wing with square center. (c) Side view, showing detachable parts. (b) (1) Tail A,…
NASA Technical Reports Server (NTRS)
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