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 13
Figure ?.- Variation of lateral-force coefficient with yaw. Rectangular NiA.C.A. 23012 wing with rounded tips in combination with olrcular fuselage; r,0°; 6f,60°.
NASA Technical Reports Server (NTRS)
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