Wing Pitching Moment Coefficient
Aircraft Engineering and Aerospace Technology
Article publication date: 1 July 1945
SCHRENK'S method for finding the wing lift distribution which has already been given in AIRCRAFT ENGINEERING can be taken further in order to determine the Pitching Moment Coefficient, CM0, about the quarter‐chord point of the mean chord at no‐lift.
Morse, W.L. (1945), "Wing Pitching Moment Coefficient", Aircraft Engineering and Aerospace Technology, Vol. 17 No. 7, pp. 204-205. https://doi.org/10.1108/eb031266
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