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 Zeit. fuer Flugtechnik und Motorluftschiffahrt, vol. 20, no. 1, Jan. 14, 1929, pp. 3-15, 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
21 pages
21 Figs.
Article (Journal)
German
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1929
|