Critical Reversal Speed

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...

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Veröffentlicht in:Aircraft Engineering and Aerospace Technology 1943-11, Vol.15 (11), p.319-324
1. Verfasser: Horton, W.H
Format: Artikel
Sprache:eng
Online-Zugang:Volltext
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Beschreibung
Zusammenfassung: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.
ISSN:0002-2667
DOI:10.1108/eb031070