Article is intended firstly, as means to quick approximate determination of critical reversal speed of wing, and, secondly, to give clearer insight of why approximations can be given for general formula for determining K, when \ill\ chord and wing chord are of linear taper at least over aileron portion.
Critical reversal speed
Aircraft Eng
Aircraft Engineering ; 15 , n 177 ; p 319-324
1943
6 pages
Article (Journal)
English
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