Propagation of Shock on NREL Phase VI Wind Turbine Airfoil under Compressible Flow
نویسندگان
چکیده
منابع مشابه
Numerical aeroelastic analysis of wind turbine NREL Phase VI Rotor
This study investigated the performance and aeroelastic characteristics of a wind turbine blade based on strongly coupled approach (two-way fluid structure interaction) to simulate the transient FSI1 responses of HAWT2. Aerodynamic response was obtained by 3D CFD-URANS approach and structural response was obtained by 3D Finite element method. Aeroelastic responses of the blade were obtained by ...
متن کاملNumerical aeroelastic analysis of wind turbine NREL Phase VI Rotor
This study investigated the performance and aeroelastic characteristics of a wind turbine blade based on strongly coupled approach (two-way fluid structure interaction) to simulate the transient FSI[1] responses of HAWT[2]. Aerodynamic response was obtained by 3D CFD-URANS approach and structural response was obtained by 3D Finite element method. ...
متن کاملnumerical aeroelastic analysis of wind turbine nrel phase vi rotor
this study investigated the performance and aeroelastic characteristics of a wind turbine blade based on strongly coupled approach (two-way fluid structure interaction) to simulate the transient fsi1 responses of hawt2. aerodynamic response was obtained by 3d cfd-urans approach and structural response was obtained by 3d finite element method. aeroelastic responses of the blade were obtained by ...
متن کاملCFD Simulation of the Flow around NREL Phase VI Wind Turbine
iv ACKNOWLEDGEMENTS I would like to express my sincere gratitude to my thesis advisor, Prof. Blair Perot, for his continuous interest, support and guidance during this study. I am also thankful to Prof. Matthew Lackner and Prof. Ashwin Ramasubramaniam for their advice and help. I specially wish to thank Chris Zusi for the all the support and great suggestions he gave me during my research as we...
متن کاملNumerical Investigation of S822 Wind Turbine Airfoil
We carried out direct numerical simulations of the flow past a two-dimensional S822 wind turbine blade section at a chord Reynolds number of Re=100,000 and an angle of attack of α = 5deg. Without blade rotation the separated boundary layer “rolls up” into spanwise vortices which then “break up” into smaller scale structures leading to transition to turbulence. Simulation results compare favorab...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Journal of Renewable Energy
سال: 2013
ISSN: 2314-4386,2314-4394
DOI: 10.1155/2013/653103