Optimum computational conditions for aerofoil simulations.
|Aerofoils||NRELS822 and NRELS823 aerofoils|
|Simulation type||Unsteady Simulation|
|Reynolds number||179 489|
|Wind speed at test section||15.8 m/s|
|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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