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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

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MCB UP Ltd

Copyright © 1943, MCB UP Limited