Primary aerodynamic factors governing performance of hovering helicopter and how necessity to operate at reasonable forward speed restricts hovering; standard power relationships for hovering flight, as developed by GLAUERT and SQUIRE. are interpreted in graphical form, and effect of formed flight in limiting choice of aerodynamic and operational parameters, due to onset of blade stalling and compressibility, is illustrated by boundaries on these graphs.
Helicopter hovering performance
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 53 , n 457
1949
10 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Helicopter stability in hovering flight
Engineering Index Backfile | 1955
|Hovering model helicopter rotor testing
NTRS | 1984
|Far-Field Analysis of Hovering Helicopter Rotor
British Library Conference Proceedings | 2015
|Helicopter control and stability in hovering flight
Engineering Index Backfile | 1948
|