include "./Mesh_1/mesh.names"
Header
CHECK KEYWORDS Warn
Mesh DB "." "Mesh_1"
Include Path ""
Results Directory ""
End
Simulation
Max Output Level = 3
Coordinate System = "Cartesian 2D"
Coordinate Mapping(3) = 1 2 3
Simulation Type = "Steady State"
Steady State Max Iterations = 10
! Output Intervals = 1
Solver Input File = "steady.sif"
Output File = "restart.res"
! Restart FIle = "restart.res"
! Restart Position = 0
End
Constants
! Gravity(4) = 0 0 -1 9.82e6 !um/s^2
Gravity(4) = 0 0 -1 9.82 !m/s^2
End
Body 1
Name = "Si"
Target Bodies(1) = $Group_1
Body Force = 1
Equation = 1
Material = 1
End
Equation 1
Name = "Fluid"
Active Solvers(1) = 1
Navier-Stokes = True
End
Solver 1
Equation = Navier-Stokes
! Flow Model = FUll
! Variable = Velocity
! Variable DOFs = 3
! Time Derivative Order = 2
Linear System Solver = Iterative
! Linear System Solver = Direct
! Linear System Symmetric = Logical True
Linear System Scaling = Logical False
Linear System Direct Method = UMFPACK
Linear System Iterative Method = BiCGStab
Linear System Convergence Tolerance = 1.0e-6
Linear System Max Iterations = 200
Linear System Preconditioning = ILU2
Nonlinear System Convergence Tolerance = Real 1.0e-7
Nonlinear System Max Iterations = Integer 100
Nonlinear System Relaxation Factor = Real 0.8
Nonlinear System Newton After Iterations = 15
Nonlinear System Newton After Tolerance = 1.0e-3
Steady State Convergence Tolerance= 1.0e-6
stabilize = True
Div Discretization = True
! Gradp Discretization = True
! Optimize Bandwidth = True
End
Material 1
Name = Air
Density = 1.0
Viscosity = 1.3e-6
! Varname Diffusivity = 1.0
End
Boundary Condition 1
Name = "Inlet"
Target Boundaries(1) = $Inlet
! Pressure = 1.00
! Temperature = 10.0
Velocity 1 = 0.005
Velocity 2 = 0
Velocity 3 = 0
End
Boundary Condition 2
Name = "Outlet"
Target Boundaries(1) = $Outlet
Pressure = 0
! Velocity 1 = 0
! Velocity 2 = 0
! Velocity 3 = -0.1
End
Boundary Condition 3
Name = "Wall"
Target Boundaries(1) = $Side
Velocity 1 = 0
Velocity 2 = 0
Velocity 3 = 0
End
Boundary Condition 4
Name = "Wall"
Target Boundaries(1) = $Circle
Velocity 1 = 0
Velocity 2 = 0
Velocity 3 = 0
End
Solver 2
Exec Solver = after all
! exec interval = 1
Equation = "ResultOutput"
Procedure = "ResultOutputSolve" "ResultOutputSolver"
Output File Name = "fluid-ss."
Output Format = vtu
Vtu Format = Logical True
! Output Format = vtk
! Vtk Format = Logical True
Vector Field 1 = Velocity
Scalar Field 1 = Pressure
! Scalar Field 2 = Absolute Magnetic Flux
! Scalar Field 3 = Equivalent Current Density 3
! Scalar Field 4 = Magnetization
End
!End Of File