!---------------------------------------------------------------- ! Test case for automated computation of boundary loads for each ! boundary. This is the most efficient way to compute fluxes when ! it is possible. There are limitations related to cases where ! nodes are shared between different boundaries. In such a case the ! procedure cannot separate between the fluxes on that node from ! different boundaries. ! ! Compared to test case "BoundaryFluxes" this hand-pics the flux to ! compute. The effect of neighbouring BCs may be omitted since they ! are natural BCs and by construction have zero flux. ! ! Similar procedure would be available through "Calculate Loads" and ! summing of nodal loads through "boundary sum" operator of SaveScalars. ! This one sweep operation is somewhat easier to use. ! ! P.R. / 26.11.2014 !----------------------------------------------------------------- Header CHECK KEYWORDS Warn Mesh DB "." "square" Include Path "" Results Directory "" End Simulation Max Output Level = 5 Coordinate System = "Cartesian" Coordinate Mapping(3) = 1 2 3 Simulation Type = "Steady State" Steady State Max Iterations = 1 Output Intervals = 1 Post File = "case.vtu" End Constants Gravity(4) = 0 -1 0 9.82 Stefan Boltzmann = 5.67e-08 End Body 1 Name = "Body" Body Force = 1 Equation = 1 Material = 1 End Equation 1 Name = "Equations" Active Solvers(2) = 1 2 End Solver 1 Exec Solver = "Always" Equation = "Heat Equation" Variable = "Temperature" Variable Dofs = 1 Linear System Solver = "Iterative" Linear System Iterative Method = "BiCGStab" Linear System Max Iterations = 350 Linear System Convergence Tolerance = 1.0e-08 Linear System Abort Not Converged = True Linear System Preconditioning = "ILU0" Linear System Residual Output = 1 Steady State Convergence Tolerance = 1.0e-05 Stabilize = True Nonlinear System Convergence Tolerance = 1.0e-05 Nonlinear System Max Iterations = 1 Nonlinear System Newton After Iterations = 3 Nonlinear System Newton After Tolerance = 1.0e-02 Nonlinear System Relaxation Factor = 1.0 Calculate Boundary Fluxes = Logical True End Solver 2 Equation = SaveScalars Procedure = "SaveData" "SaveScalars" ! This will make the heat flux through boundary 3 the value ! to monitor in the consistency test. SaveScalars is only needed ! to implement the test, not to compute the flux. Show Norm Index = 1 ! Filename = f.dat End Material 1 Name = "Material" Density = 1 Heat Conductivity = 10.0 End Body Force 1 Name = "BodyForce" Heat Source = 0 End Boundary Condition 1 Name = "Bot" Target Boundaries(1) = 1 Temperature = 0.0 End Boundary Condition 2 Name = "Right" Target Boundaries(1) = 2 End Boundary Condition 3 Name = "Top" Target Boundaries(1) = 3 Temperature = 10.0 ! Hand-pick only this BC to be computed Calculate Boundary Flux = Logical True End Boundary Condition 4 Name = "Left" Target Boundaries(1) = 2 End Solver 2 :: Reference Norm = Real 100.0 RUN !End Of File