Table 1: Adopted Boundary Conditions - It was through the boundary conditions that the defined properties of the fluid will be calculated.
Boundaries |
Boundary conditions |
Inlet and top & bottom boundaries |
Homogeneous velocity profile , with adjustable velocity components u and v as needed, and the component w with zero velocity. |
Outlet |
Static pressure equal to 0 Pa, or gauge pressure equal to atmospheric pressure. |
Airfoil-wall |
No-slip condition, impermeable wall, stationary wall. |
Fluid |
Atmospheric air as the working fluid used with a constant density of 1.225 kg/m^{3} and a viscosity of 1.7894 × 10^{-5} kg/m·s |