It has been shown by the calculations of a preceding note that the effect on the lift of a rotor due to an increase in the effective collective pitch, while in the course of steady descending vertical flight near the autorotative regime, depends essentially upon the speed of the pitch change. Experiment confirms the result.
Wind-Tunnel Study of the Response in Lift of a Rotor to an Increase in Collective Pitch in the Case of Vertical Flight Near the Autorotative Regime
1960
8 pages
Report
No indication
English
Engineering Index Backfile | 1960
|Engineering Index Backfile | 1960
|Response of helicopter rotor to increase in collective pitch for case of vertical flight
Engineering Index Backfile | 1961
|