This paper deals with a second-order perturbation analysis of the in-plane dynamic responses of both tuned and mistuned three-blade-hub horizontal-axis wind-turbine equations. The blades are under effect of gravitational and cyclic aerodynamics forces and centrifugal forces. Although the blades and hub equations are coupled, they can be decoupled by changing the independent variable from time to rotor angle and by using a small parameter approximation. A second-order method of multiple scales is applied in the rotor-angle domain to analyze in-plane blade-hub dynamics. A superharmonic resonance case at one third the natural frequency was revealed. This resonance case was not captured by a first-order perturbation expansion. The relationship between response amplitude and frequency is studied. The effect of blade mistuning on the coupled blade-hub dynamics are taken into account.
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ASME 2018 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
August 26–29, 2018
Quebec City, Quebec, Canada
Conference Sponsors:
- Design Engineering Division
- Computers and Information in Engineering Division
ISBN:
978-0-7918-5185-2
PROCEEDINGS PAPER
Second-Order Perturbation Analysis of In-Plane Blade-Hub Dynamics of Horizontal-Axis Wind Turbines
Ayse Sapmaz,
Ayse Sapmaz
Michigan State University, East Lansing, MI
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Brian F. Feeny
Brian F. Feeny
Michigan State University, East Lansing, MI
Search for other works by this author on:
Ayse Sapmaz
Michigan State University, East Lansing, MI
Brian F. Feeny
Michigan State University, East Lansing, MI
Paper No:
DETC2018-86203, V008T10A027; 9 pages
Published Online:
November 2, 2018
Citation
Sapmaz, A, & Feeny, BF. "Second-Order Perturbation Analysis of In-Plane Blade-Hub Dynamics of Horizontal-Axis Wind Turbines." Proceedings of the ASME 2018 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. Volume 8: 30th Conference on Mechanical Vibration and Noise. Quebec City, Quebec, Canada. August 26–29, 2018. V008T10A027. ASME. https://doi.org/10.1115/DETC2018-86203
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