Wing Pressure Distribution and Rotor-Blade Motion of an Autogiro as Determined in Flight (1935)
NASA Technical Reports Server (NTRS) · leaf 10
sed a limit upon the severity with turn possibly influences the blade motion. which the test pilot performed the maneuver. During Accelerated flight.—At the beginning of the accel- these tests, ;i change in instrument installation resulted erated-flighl tests it had been planned to obtain data in a… … Timej seconds Time, seconds Figure 15.—Time history of abrupt turn, Fo=106 m.p.h. Weight = 2,9.50 lb. Figure 17.- -Time history of abrupt turn, Vb=116 m.p.h. Weight=2,900 lb. (PCA-2 autogiro). (PCA-2 autogiro). ISO WO \ ^100 100 50 o 12 8 4 0 4 6 12 12 8 4 0 4 8 12 Right Distance along span from…
NASA Technical Reports Server (NTRS)
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