Results of flight test carried on by Deutsche Versuchsanstalt fuer Luftfahrt to determine effect of structural features of airplane on its stability, controllability, maneuverability and spinning characteristics; synopsis of flight tests from 1925-1927; information obtained from 1927-1928 flight tests; causes of flat spins; importance of damping action of vertical tail surfaces during spin; problems for 1928-1929, flight tests. From Zeit. fuer Flugtechnik und Motorluftschiffahrt, Apr. 29, 1929.
Information obtained from airplane flight tests in the year 1927-1928
Nat Advisory Committee Aeronautics -- Tech Memo
1929
24 pages
9 Supp. figs.
Aufsatz (Zeitschrift)
Englisch
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