Wind-tunnel investigation of effect of yawing on lateral-stability characteristics II : rectangular N.A.C.A. 23012 wing with a circular fuselage
A 1939 NASA technical report, a wind-tunnel study of yawing effects on lateral stability for a rectangular N.A.C.A. 23012 wing on a circular fuselage, written for aeronautical engineers. Its pictures are plotted graphs of a yawing-moment coefficient against angle of attack, with curves for wing locations high, mid and low, fin on and off, and wing alone, which a designer might use as a model for reading comparative trend data across configurations.
