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Table 2

Optimum computational conditions for aerofoil simulations.

Aerofoils NRELS822 and NRELS823 aerofoils
Simulation type Unsteady Simulation
Fluid material Air
Temperature 288 K
Kinematic viscosity
Reynolds number 179 489
Density 1.225 kg/m3
Wind speed at test section 15.8 m/s
Turbulent model (4eqn)
Inlet and outlet static pressure −149.4 Pa
Inlet intermittency gamma (γ) 1
Inlet turbulent intensity 5%
The angle of attack (AoA) 18°

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