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Dynamics of Rotors Operating at High Advance Ratios
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Dynamics of Rotors Operating at High Advance Ratios
Dynamics of Rotors Operating at High Advance Ratios
GS
G. J. Sissingh
G. J. Sissingh
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1 July 1968
journal article
Published by
AHS International dba Vertical Flight Society
in
Journal of the American Helicopter Society
Vol. 13
(3)
,
56-63
https://doi.org/10.4050/jahs.13.3.56
Abstract
The rotor blade represents a spring‐mass‐damper system with periodically changing spring and damper characteristics which is excited by aerodynamic forces due to inflow, blade twist, and cyclic and collective pitch.
Keywords
SPRING
TWIST
CYCLIC
PITCH
AERODYNAMIC
INFLOW
DAMPER
EXCITED
ROTORS OPERATING
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