sunfluidh:2d_channel_flow_with_heated_bar_incomp_flow
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=========================================================================== =========================================================================== MAIN INPUT DATA FILE : 2D CHANNEL FLOW WITH A SQUARE BAR (OBSTACLE) INCOMPRESSIBLE FLOW HEATED SQUARE BAR AT TEMPERATURE Th = 2.Tc OTHER WALLS AT Tc TEMPERATURE OF THE INFLOW : Tc GRAVITY & BUOYANCY ARE NEGLECTED DIMENSIONLESS LAYOUT : Length scale : h (the channel height) Reynolds number Re_h= rho_0.U_0.h/nu= 100 dimensionless quantities : velocity U* = U/U_0 temperature T*= T/T0 with T0= Tc ---> Tc*= 1 and Th*= 2 kinetic viscosity= 1/Re_h dimensionless domain : Lx/h= 10 Initialisation = uniform velocity field inlet flowrate = uniform profil INCOMPRESSIBLE DOWNSTEP FLOW Tc ------------------------------------------ |Th| |__| ---> inflow outflow ---> (Tc) ------------------------------------------ Tc J ^ | | ---->I =========================================================================== =========================================================================== &Version File_Version="VERSION2.0"/ ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ GENERAL LAYOUT (DIMENSIONLESS) ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ &Fluid_Properties Reference_Dynamic_Viscosity = 1.00D-02, Reference_Density= 1.0 , Reference_Temperature= 1.0 / &Velocity_Initialization I_Velocity_Reference_Value = 1.0 , J_Velocity_Reference_Value = 0.0 , K_Velocity_Reference_Value = 0.0 / =========================================================================== DOMAIN FEATURES (DIMENSIONLESS) =========================================================================== &Domain_Features Start_Coordinate_I_Direction= 0.00 , End_Coordinate_I_Direction= 10.00, Start_Coordinate_J_Direction= 0.00 , End_Coordinate_J_Direction= 1.00, Start_Coordinate_K_Direction= 0.00 , End_Coordinate_K_Direction= 0.00, Cells_Number_I_Direction= 256 ,Cells_Number_J_Direction= 64 ,Cells_Number_K_Direction= 1, Regular_Mesh= .true. / ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ DEFINITION OF BOUNDARY CONDITIONS ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ============================================================================= WALL BOUNDARY CONDITION SETUP (DIMENSIONLESS) ============================================================================= --------------------------------------------------- DATA SET FOR THE WALL BOUNDARY CONDITIONS --------------------------------------------------- First set of wall boundary conditions (applied to the walls of the channel) : imposed temperature : Tc -------- &Heat_Wall_Boundary_Condition_Setup West_Heat_BC_Option = 0 , East_Heat_BC_Option = 0 , Back_Heat_BC_Option = 0 , Front_Heat_BC_Option = 0 , West_Wall_BC_Value= 1.0 , East_Wall_BC_Value= 1.0 , Back_Wall_BC_Value= 1.0 , Front_Wall_BC_Value= 1.0 / The usual wall boundary conditions for the velocity are used (no-slip and impermeability conditions). As they are the conditions by default, they are not explicitly written -------- Second set of wall boundary conditions (applied to the walls of the square bar) : imposed temperature : Th -------- &Heat_Wall_Boundary_Condition_Setup West_Heat_BC_Option = 0 , East_Heat_BC_Option = 0 , Back_Heat_BC_Option = 0 , Front_Heat_BC_Option = 0 , West_Wall_BC_Value= 2.0 , East_Wall_BC_Value= 2.0 , Back_Wall_BC_Value= 2.0 , Front_Wall_BC_Value= 2.0 , End_of_Data_Block= .true. / The usual wall boundary conditions for the velocity are used (no-slip and impermeability conditions). As they are the conditions by default, they are not explicitly written ------------------------------------------------------- GEOMETRY OF THE IMMERSED BODIES ------------------------------------------------------- First (and unic) immersed body (temperature Th= 2.Tc) &Polyhedral_Immersed_Bodies Xi_1= 4.5 , Xj_1= 0.5 ,Xk_1= 0.0 , Xi_2= 5.5 , Xj_2= 0.5 ,Xk_2= 0.0 , Xi_3= 5.5 , Xj_3= 1.0 ,Xk_3= 0.0 , Xi_4= 4.5 , Xj_4= 1.0 ,Xk_4= 0.0 , Identifier_Value= 2, End_of_Data_Block= .true. / ============================================================================= INLET AND OUTLET BOUNDARY CONDITIONS (DIMENSIONLESS) ============================================================================= Inlet : Uniform flowrate profil &Inlet_Boundary_Conditions Type_of_BC= "INLET", Direction_Normal_Plan= 1 , Flow_Direction= 1 , Plan_Location_Coordinate= 0.0 , Start_Coordinate_of_First_Span = 0.00 , End_Coordinate_of_First_Span = 1.00 , Start_Coordinate_of_Second_Span= 0.0 , End_Coordinate_of_Second_Span= 0.0 , Normal_Velocity_Reference_Value= 1.0 , Temperature_Reference_Value= 1.0 , End_of_Data_Block= .true. / &Outlet_Boundary_Conditions Type_of_BC= "OUTLET", Direction_Normal_Plan= 1 , Flow_Direction= 1 , Plan_Location_Coordinate= 10.0 , Start_Coordinate_of_First_Span = 0.00 , End_Coordinate_of_First_Span = 1.00 , Start_Coordinate_of_Second_Span= 0.0 , End_Coordinate_of_Second_Span= 0.0 , End_of_Data_Block= .true. / ============================================================================= BORDER BOUNDARY CONDITIONS ============================================================================= !--- No change &Border_Domain_Boundary_Conditions West_Border= 0 , East_Border= 0 , Back_Border= 0 , Front_Border= 0 , North_Border = 0 , South_Border = 0 / ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ NUMERICAL METHODS ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ For Navier-Stokes Equations : Numerical scheme --> BDF2 - Spatial discretization --> 2nd order centered scheme convection flux ---> conservative form For Poisson's equation : Iterative method --> SOR coupled with a multigrid method. Parameters of the multigrid method : &Numerical_Methods Numerical_Scheme= 1 , Convective_Flux_Discretization_Type = 1 Numerical_Method_Poisson_Equation= 1, Number_max_Grid= 4 , Number_max_Cycle= 10 , Number_Iteration= 15 , Relaxation_Coefficient = 1.80 , Convergence_Criterion = 1.D-08 / ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ SIMULATION MANAGEMENT ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ The numerical time step is imposed &Simulation_Management Restart_Parameter= 0 , Steady_Flow_Stopping_Criterion_Enabled = .true. , Steady_Flow_Stopping_Criterion = 1.D-16, Temporal_Iterations_Number = 100000 , Final_Time = 5.D+02 , TimeStep_Type = 0 , Timestep_Max = 1.D-03 , Simulation_Backup_Rate = 1000 , Simulation_Checking_Rate = 101 / ============================================================================= PROBES MANAGEMENT ============================================================================= Probes order U , V , W , T , P , RHO &Probe_Quantities_Enabled Temporal_Series_For_Quantity_Enabled(:) = .true., .true., .false., .false., .true. , .false. / &Probe_Location Xi= 3.0 , Xj= 0.5 , Xk= 0.0 / &Probe_Location Xi= 6.0 , Xj= 0.5 , Xk= 0.0 , End_of_Data_Block= .true. / &Simulation_Management Probe_Recording_Rate = 10 / ============================================================================= FIELDS RECORDING DECLARATION ============================================================================= &Field_Recording_Setup Precision_On_Instantaneous_Fields= 2 / !--- Snapshots &Simulation_Management Fields_Recording_Rate = 5.D+01 / &Instantaneous_Fields_Listing Name_of_Field = "U " , Recording_Enabled = .true. / First velocity component &Instantaneous_Fields_Listing Name_of_Field = "V " , Recording_Enabled = .true. , End_of_Data_Block= .true / Second velocity component !--- Statistics &Simulation_Management Start_Time_For_Statistics= 1.D+03 , Time_Range_Statistic_Calculation = 5.D+00 / &Statistical_Fields_Listing Name_of_Field = "<U> " , Recording_Enabled = .true. / &Statistical_Fields_Listing Name_of_Field = "<V> " , Recording_Enabled = .true. , End_of_Data_Block= .true /
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sunfluidh/2d_channel_flow_with_heated_bar_incomp_flow.1480502066.txt.gz · Dernière modification : 2016/11/30 11:34 de yann