Tentative method presented depends upon use of strip theory, in manner of E.G.BROADBENT, and calculation of lift distribution in transonic range for wings in roll, as suggested by K.W.MANGLER; aileron reversal criterion in transonic case.
Note on problems of aileron reversal at transonic speeds
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 57 , n 508
1953
4 pages
Aufsatz (Zeitschrift)
Englisch
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Calculation of transonic aileron buzz
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