Analysis of flight and wind-tunnel tests on Udet airplanes with reference to spinning characteristics (1929)
NASA Technical Reports Server (NTRS) · leaf 33
N.A.C A. Teclmical Meruoro^ndmri Mo. 503 FigG.16 & 17 High v/ing U7 … Fig.16 U7 Spinning tests. The aileron defloction and speed increase the angular velocity. Biplane U12 IJ V Fig.17 U12 Spinning tests.Here the angular velocity is a rninim-uiTi for angular deflection, pq = 0,a,nd a maximum for p = 20^.Their orders of magnitude agree fairly well rrth the flight-tests…
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