To read the full version of this content please select one of the options below:

Lift‐Curve Slope at Subsonic and Supersonic Speeds: Graphical Presentation of Theoretical Results for Straight‐Tapered Wings

A. Stanbrook B.Sc., M.I.A.S. (National Aeronautical Establishment, Bedford.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 August 1954

152

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

Related articles