Abstract
The unsteady flow around a pitching two-dimensional airfoil section (NREL S809) has been simulated using unsteady RANS with the transition SST turbulence model. This geometry is chosen to represent a wind turbine blade in a standstill configuration. The Reynolds number is Re=106 based on a chord length of 1 m. A prescribed sinusoidal pitching motion has been applied at a fixed amplitude of 7° for a range of high angles of attack 30°
Cite
CITATION STYLE
Meskell, C., & Pellegrino, A. (2019). Vortex shedding lock-in due to pitching oscillation of a wind turbine blade section at high angles of attack. International Journal of Aerospace Engineering, 2019. https://doi.org/10.1155/2019/6919505
Register to see more suggestions
Mendeley helps you to discover research relevant for your work.
