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Wing Lift Distribution

Wing Lift Distribution THE present article is the application of Schrenk's approximate method to two cases, one a wing without twist and the other the same wing with twist, the nomenclature of Schrenk's article having been altered to conform to British usage, and a certain amount of explanatory matter added in order to make the method more easily understood. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031125
Publisher site
See Article on Publisher Site

Abstract

THE present article is the application of Schrenk's approximate method to two cases, one a wing without twist and the other the same wing with twist, the nomenclature of Schrenk's article having been altered to conform to British usage, and a certain amount of explanatory matter added in order to make the method more easily understood.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: May 1, 1944

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