It is shown by calculation of preceding note that effect on lift of rotor due to increase in effective collective pitch, while in course of steady descending vertical flight near autorotative regime, depends essentially upon speed of pitch change; experiment confirms result. Translated from Acad des Sciences -- Comptes Rendus Sept 8 1958.
Wind-tunnel study of response in lift of rotor to increase in collective pitch in case of vertical flight near autorotative regime
NASA -- Tech Translation
1960
4 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1960
|Response of helicopter rotor to increase in collective pitch for case of vertical flight
Engineering Index Backfile | 1961
|