Case Study #3: Nonlinear Aeroelasticity
作者： Rush D. Robinett , David G. Wilson
DOI: 10.1007/978-0-85729-823-2_8
关键词:
摘要: Chapter 8 applies HSSPFC to a nonlinear stall flutter problem. A aerodynamic and structural model is developed that representative of the first torsional mode nominal 5 MW rated power wind turbine blade. This analyzed using determine limit cycle behavior condition mode. Also, this further effectiveness feedback control on suppression demonstrate defines stability boundary. analysis serves as foundation for investigation large dynamic conditions. The closer can safely operate stall, greater energy capture.
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