Critical Reversal Speed
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 November 1943
Abstract
THIS article is intended, firstly, as a means to a quick approximate determination of the critical reversal speed of a wing, and secondly to give a clearer insight of why approximations can be given for the general formula for determining K, when the aileron chord and wing chord are of linear taper at least over the aileron portion.
Citation
Horton, W.H. (1943), "Critical Reversal Speed", Aircraft Engineering and Aerospace Technology, Vol. 15 No. 11, pp. 319-324. https://doi.org/10.1108/eb031070
Publisher
:MCB UP Ltd
Copyright © 1943, MCB UP Limited