Critical Reversal Speed

descriptionPublicationkeyboard_double_arrow_right Article 01 Nov 1943 English Publisher:EmeraldJournal:Aircraft Engineering and Aerospace Technology, volume 15, pages 319-324 (issn: 0002-2667,

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Authors: W.H. Horton;

doi: 10.1108/eb031070

Critical Reversal Speed

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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.

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