Wing Pitching Moment Coefficient

Abstract

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.

Citation

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