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Wing Pitching Moment Coefficient

Wing Pitching Moment Coefficient 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 quarterchord point of the mean chord at nolift. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Wing Pitching Moment Coefficient

Aircraft Engineering and Aerospace Technology , Volume 17 (7): 2 – Jul 1, 1945

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031266
Publisher site
See Article on Publisher Site

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 quarterchord point of the mean chord at nolift.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Jul 1, 1945

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