NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Whirl flutter analysis of a horizontal-axis wind turbine with a two-bladed teetering rotorWhirl flutter and the effect of pitch-flap coupling on teetering motion of a wind turbine were investigated. The equations of motion are derived for an idealized five-degree-of-freedom mathematical model of a horizontal-axis wind turbine with a two-bladed teetering rotor. The model accounts for the out-of-plane bending motion of each blade, the teetering motion of the rotor, and both the pitching and yawing motions of the rotor support. Results show that the design is free from whirl flutter. Selected results are presented indicating the effect of variations in rotor support damping, rotor support stiffness, and pitch-flap coupling on pitching, yawing, teetering, and blade bending motions.
Document ID
19820015831
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Janetzke, D. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Kaza, K. R. V.
(Toledo Univ.)
Date Acquired
August 10, 2013
Publication Date
May 1, 1981
Publication Information
Publication: NASA. Lewis Research Center Wind Turbine Dyn.
Subject Category
Energy Production And Conversion
Accession Number
82N23707
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available