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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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