Research Article
Comparative Study and Aerodynamic Analysis of Rectangular Wing Using High-Lift Systems
Table 2
Solver details and boundary conditions.
(a) |
| | Solver details | | Solver | Pressure based-coupled |
| | Turbulence model | SST K-omega | | Fluid | Air | | Flow condition | Steady state | | Convergence criteria | 1.00E-06 |
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(b) |
| | Boundary conditions | | Inlet | Velocity inlet |
| | Outlet | Pressure outlet | | Symmetry | Symmetry | | Farfield | Slip wall (inviscid wall) | | Wing surface | No-slip wall (viscous wall) |
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