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Wing Pitching Moment Coefficient

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1945

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

Publisher

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MCB UP Ltd

Copyright © 1945, MCB UP Limited