Piv experimental and numerical study of a 2-D airfoil for wind turbines

Author

Jing, Ma ; Rui, Guo ; Jinglei, Xu ; Kunyuan, Zhang

Author_Institution

Coll. of Energy & Power Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China

fYear

2009

fDate

24-26 Sept. 2009

Firstpage

1

Lastpage

6

Abstract

The 2-D airfoil of the wind turbine (NREL S809) was experimentally and numerically studied. The experiment focused on the PIV measurement of the 2-D airfoil flow field with different angles of attack under various Reynolds numbers. A lot of important and useful information was obtained. Furthermore, the experimental result was compared with CFD simulation in order to study the flow field in more detail, especially the useful graphs of the velocity vector, the data of the lift and drag, the distribution of the vortex, and separation of surface boundary layer under the different angles of attack and with different Reynolds numbers were compared and analyzed. Relatively good agreement between the experimental and numerical result was achieved.

Keywords

numerical analysis; wind turbines; 2D airfoil; CFD simulation; NREL S809; PIV measurement; Reynolds numbers; numerical study; surface boundary layer; velocity vector; wind turbines; Aerodynamics; Automotive components; Blades; Computational fluid dynamics; Power engineering and energy; Rough surfaces; Surface roughness; Wheels; Wind energy; Wind turbines; CFD; PIV; boundary layer separation; drag coefficient; lift coefficient; stall; velocity vector; vortex;

fLanguage

English

Publisher

ieee

Conference_Titel

World Non-Grid-Connected Wind Power and Energy Conference, 2009. WNWEC 2009

Conference_Location

Nanjing

Print_ISBN

978-1-4244-4702-2

Type

conf

DOI

10.1109/WNWEC.2009.5335839

Filename

5335839