Wind-tunnel investigation of effect of yawing on lateral-stability characteristics II : rectangular N.A.C.A. 23012 wing with a circular fuselage (1939)
NASA Technical Reports Server (NTRS) · leaf 16
N.A.C.A. Teohnioal Note Ho. 730 Figs.12,13 … Angle of attack,a,deg. Figure 12.- Variation of^^r) with angle of attack. Rectangular H.A.O.A. 23012 wing alone and in combination with oiroular fuselage with and without fin; 6f,60°; r,6°. 1 1 1 1 1 Wing location.High Hid Low Fin on + d > .006 Fin off O v x Wing alone A O < e.g. 004 .003 -.002 5…
NASA Technical Reports Server (NTRS)
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