Results of tests with light biplane, high-wing monoplane, and low-wing monoplane discussed; systematic spinning tests using two rudders, one enlarged backward and other upward; wind-tunnel tests; comparison of inertia forces inspinning with aerodynamic longitudinal or pitching moment. (see also translation in Nat. Advisory Committee for Aeronautics -- Tech. Memorandum, no. 502, Mar. 1929, 21 pp., 21 figs., partly on supp. plates)
Analysis of flight and wind-tunnel tests on udet airplanes with reference to spinning characteristics
Low-wing Udet U 6, Udet U 7 "Kolibri," Udet U 12 "Flamingo." (Auswertung von Flugversuchen und Windkanalmessungen an den Udet-Flugzeugen)
1929
13 pages
21 Figs.
Article (Journal)
German
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Engineering Index Backfile | 1929
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