Open AccessFlap/lead–lag aeroelastic stability of wind turbine blade sections
Author(s) -
Chaviaropoulos P. K.
Publication year - 1999
Publication title -
wind energy
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.743
H-Index - 92
eISSN - 1099-1824
pISSN - 1095-4244
DOI - 10.1002/(sici)1099-1824(199904/06)2:2<99::aid-we21>3.0.co;2-u
Subject(s) - aeroelasticity , aerodynamics , turbine blade , structural engineering , flutter , vibration , turbine , engineering , context (archaeology) , aerodynamic force , helicopter rotor , damper , control theory (sociology) , computer science , rotor (electric) , mechanical engineering , aerospace engineering , geology , physics , acoustics , paleontology , control (management) , artificial intelligence
The scope of this article is to investigate the aeroelastic stability of wind turbine blade sections subjected to combined flap/lead–lag motion. The work is motivated by recent concern about destructive ‘edgewise' vibrations of modern, half‐megawatt‐scale, blades. The aeroelastic governing equations derive from the combination of a spring–mass–damper equivalent of the structure and a ‘non‐stationary' aerodynamic model. The aerodynamic model used in the present context is the differential dynamic stall model developed at ONERA. The resulting equations of motion are linearized and their stability characteristics are investigated in terms of the system entries, expressed through suitable, non‐dimensional, structural and aerodynamic parameters. Copyright © 1999 John Wiley & Sons, Ltd.