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LiftCurve Slope at Subsonic and Supersonic Speeds

LiftCurve Slope at Subsonic and Supersonic Speeds Theoretical results for the initial liftcurve slope of straighttapered wings, based on the linearized equations of inviscid motion, have been evaluated and are presented in the form of graphs. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

LiftCurve Slope at Subsonic and Supersonic Speeds

Aircraft Engineering and Aerospace Technology , Volume 26 (8): 14 – Aug 1, 1954

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb032455
Publisher site
See Article on Publisher Site

Abstract

Theoretical results for the initial liftcurve slope of straighttapered wings, based on the linearized equations of inviscid motion, have been evaluated and are presented in the form of graphs.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Aug 1, 1954

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