Air forces and air-force moments at large angles of attack and how they are affected by the shape of the wing (1930)
NASA Technical Reports Server (NTRS) · leaf 25
N.A.C.A. Technical Memoramdvim No.573 j.14,15,16 -4^0.368 —* / 1,0.164 Profile of 112 3=0.055 -V0.168. fig. 14 Profile of the staggered biplane tings of 1.2 m span and 0.38 m2 total area. … Pig. 16 Moment about the fuselage axis plotted against the angle of attack and bj»x for the staggered biplane wing-of Fig* 14. 2v
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