Aerodynamic behaviour of NREL S826 airfoil at Re=100,000

The Science of Making Torque from Wind 2014

Sarlak, H.^1 ; Mikkelsen, R.^1 ; Sarmast, S.^1,2 ; Sørensen, J.N.^1

Technical University of Denmark, DK-2800 Lyngby, Denmark^1

Swedish E-Science Research Centre (SeRC), Linne FLOW Centre, Royal Institute of Technology, SE-100 44 Stockholm, Sweden^2

关键词: Gauge measurements;    High angles of attack;    Lift coefficient;    Low-speed wind tunnel;    Mechanics laboratory;    Numerical computations;    Technical University of Denmark;    Wind tunnel measurements;   

Others  :  https://iopscience.iop.org/article/10.1088/1742-6596/524/1/012027/pdf
DOI  :  10.1088/1742-6596/524/1/012027

来源: IOP

【 摘 要 】

This paper presents wind tunnel measurements of the NREL S826 airfoil at Reynolds number Re 100,000 for angles of attack in a range of -10° to 25° the corresponding Large Eddy Simulation (LES) for selected angles of attack. The measurements have been performed at the low speed wind tunnel located at Fluid Mechanics laboratory of the Technical University of Denmark (DTU). Lift coefficient is obtained from the forge gauge measurements while the drag is measured according to the integration of the wake profiles downstream of the airfoil. The pressure distribution is measured by a set of pressure taps on the airfoil surface. The lift and drag polars are obtained from the LES computations using DTU's inhouse CFD solver, EllipSys3D, and good agreement is found between the measurement and the simulations. At high angles of attack, the numerical computations tend to over-predict the lift coefficients, however, there is a better agreement between the drag measurements and computations. It is concluded that LES computations are able to capture the lift and drag polars as well as the pressure distribution around the airfoil with an acceptable accuracy.