Analysis of flight and wind-tunnel tests on Udet airplanes with reference to spinning characteristics (1929)
NASA Technical Reports Server (NTRS) · leaf 25
N.A.C.A.- Technical Memorandura No.503 Figs.4 & 12. /y / Coxmter Center of 7^ gravity x Fig.4 Installation for spinning test in wind tiinnel. Rudder Low wing U6 deflection … Fig. 12 Effectiveness- of ailerons and rudders on U6 a.nd U7. The rudder forces and moments a.re greater on the high wing monoplane. Bet:7een 10^ and 22^ angle of attack the aalerons of U7 are superior "beoouse they produce larger rolling moments and smaller yawing moments, The smaller yawing…
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