From: Experimental and numerical study of novel Coanda-based unmanned aerial vehicle
Solver settings | |
Type | Pressure based |
Velocity formulation | Absolute |
Time | Steady |
Models | |
Energy equation | Disabled |
Turbulence model | k-ϵ realizable |
Near-wall treatment | Scalable wall functions |
Materials | |
Fluid | Air |
Density | 1.225 kg/m3 |
Viscosity | 0.000017894 kg/m.s |
Cell zone conditions | |
Rotating domain | Frame motion |
Rotating axis direction | X-axis |
Boundary conditions | |
Inlet | Pressure inlet |
Outlet | Pressure outlet |
Propeller | Moving wall (rotation along x-axis) |
Domain walls | Walls |
Solution settings | |
Pressure-velocity coupling scheme | SIMPLE |
Gradient | Least-squares cell based |
Pressure | Second order |
Momentum | Second order |
Turbulent kinetic energy | Second-order upwind |
Turbulent dissipation rate | Second-order upwind |
Initialization | Standard initialization |