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Wind-tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics I : Four N.A.C.A. 23012 Wings of Various Plan Forms with and Without Dihedral (1939) NASA Technical Reports Server (NTRS) · leaf 13
Fig. 7 N.A.C.A. Technical Note Ho. 703 .03 Angle of yaw, ,deg. (a) r, 0°; 6f, 0° (o) r, 5°; 6f, 0° NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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