Analysis of flight and wind-tunnel tests on Udet airplanes with reference to spinning characteristics (1929)
NASA Technical Reports Server (NTRS) · leaf 23
A.C.A. TechniCcal Memora,ndum No. 502 Fig.2 H 02 r3200 nun … 1050 mm Fig,2 U7.Kolibri high wing airplane.20 HP engine.Iseat. The change in position of center of gravity d"j« % the^ enlarging and the fitting of a different (Siemens), engine made necessary e;a entirely different type of con- struction. The vertical fin and rudder used on the wind tunnel model…
NASA Technical Reports Server (NTRS)
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