Theoretical analysis of oscillations in hovering of helicopter blades with inclined and offset flapping and lagging hinge axes.
Theoretical analysis of oscillations in hovering of helicopter blades with inclined and offset flapping and lagging hinge axes
Nat Advisory Committee Aeronautics -- Tech Note
1950
31 pages
Diagrs, tables
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Online Contents | 2008
Hovering Hinge-Connected-Flapping Plate with Passive Deflection (TN)
Online Contents | 2012
|Analyzing Wakes From Hovering-Helicopter Rotor Blades
NTRS | 1987
|