Lift‐Curve Slope at Subsonic and Supersonic Speeds: Graphical Presentation of Theoretical Results for Straight‐Tapered Wings
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 August 1954
Abstract
Theoretical results for the initial lift‐curve slope of straight‐tapered wings, based on the linearized equations of inviscid motion, have been evaluated and are presented in the form of graphs.
Citation
Stanbrook, A. (1954), "Lift‐Curve Slope at Subsonic and Supersonic Speeds: Graphical Presentation of Theoretical Results for Straight‐Tapered Wings", Aircraft Engineering and Aerospace Technology, Vol. 26 No. 8, pp. 244-257. https://doi.org/10.1108/eb032455
Publisher
:MCB UP Ltd
Copyright © 1954, MCB UP Limited