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Merge pull request #11 from su2code/develop
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‎incompressible_flow/Inc_Heated_Cylinders/mesh_cht_3cyl.su2

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‎incompressible_flow/Inc_Streamwise_Periodic/chtPinArray_2d.geo

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‎incompressible_flow/Inc_Streamwise_Periodic/fluid_FFD.su2

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‎incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_dp_hf_tp.cfg

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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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% %
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% SU2 configuration file %
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% Case description: Unit Cell flow around pin array (fluid) %
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% Author: T. Kattmann %
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% Institution: Robert Bosch GmbH %
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% Date: 2020.12.15 %
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% %
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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%
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% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
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%
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SOLVER= INC_RANS
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KIND_TURB_MODEL= SST
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%
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% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
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%
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INC_DENSITY_MODEL= CONSTANT
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INC_DENSITY_INIT= 1045.0
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INC_VELOCITY_INIT= ( 0.1, 0.0, 0.0 )
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%
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INC_ENERGY_EQUATION = YES
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INC_TEMPERATURE_INIT= 338.0
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INC_NONDIM= DIMENSIONAL
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SPECIFIC_HEAT_CP= 3540.0
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%
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FREESTREAM_TURBULENCEINTENSITY= 0.05
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FREESTREAM_TURB2LAMVISCRATIO= 10.0
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%
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% --------------------------- VISCOSITY MODEL ---------------------------------%
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%
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VISCOSITY_MODEL= CONSTANT_VISCOSITY
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MU_CONSTANT= 0.001385
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%
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% --------------------------- THERMAL CONDUCTIVITY MODEL ----------------------%
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%
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% Pr_lam = mu_lam [Pa*s] * c_p [J/(kg*K)] / lambda[W/(m*K)]
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% = 1.385e-3 * 3540 / 0.42
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% = 11.7
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CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
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PRANDTL_LAM= 11.7
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%
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TURBULENT_CONDUCTIVITY_MODEL= CONSTANT_PRANDTL_TURB
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PRANDTL_TURB= 0.90
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%
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% --------------------- STREAMWISE PERIODICITY DEFINITION ---------------------%
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%
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KIND_STREAMWISE_PERIODIC= PRESSURE_DROP
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STREAMWISE_PERIODIC_PRESSURE_DROP= 208.023676
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%
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STREAMWISE_PERIODIC_TEMPERATURE= YES
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%
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% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
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%
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MARKER_HEATFLUX= ( fluid_pin1_interface, 5e5, \
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fluid_pin2_interface, 5e5, \
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fluid_pin3_interface, 5e5 )
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MARKER_SYM= ( fluid_symmetry )
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MARKER_PERIODIC= ( fluid_inlet, fluid_outlet, 0.0,0.0,0.0, 0.0,0.0,0.0, 0.0111544,0.0,0.0 )
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%
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% Alternative to periodic simulation with velocity inlet and pressure outlet
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%INC_INLET_TYPE= VELOCITY_INLET
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%MARKER_INLET= ( fluid_inlet, 338.0, 0.75, 1.0, 0.0, 0.0 )
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%INC_OUTLET_TYPE= PRESSURE_OUTLET
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%MARKER_OUTLET= ( fluid_outlet, 0.0 )
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%
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% ------------------------ SURFACES IDENTIFICATION ----------------------------%
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%
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MARKER_MONITORING= ( fluid_pin2_interface )
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%
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MARKER_ANALYZE = ( fluid_outlet, fluid_inlet )
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MARKER_ANALYZE_AVERAGE = MASSFLUX
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%
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% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
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%
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ITER= 3500
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NUM_METHOD_GRAD= GREEN_GAUSS
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CFL_NUMBER= 1e2
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%
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% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
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%
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LINEAR_SOLVER= FGMRES
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LINEAR_SOLVER_PREC= ILU
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LINEAR_SOLVER_ERROR= 1e-3
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LINEAR_SOLVER_ITER= 20
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%
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% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
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%
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CONV_NUM_METHOD_FLOW= FDS
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MUSCL_FLOW= YES
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SLOPE_LIMITER_FLOW= NONE
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%
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TIME_DISCRE_FLOW= EULER_IMPLICIT
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%
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% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
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%
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CONV_NUM_METHOD_TURB= SCALAR_UPWIND
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MUSCL_TURB= NO
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SLOPE_LIMITER_TURB= NONE
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%
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TIME_DISCRE_TURB= EULER_IMPLICIT
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%
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% --------------------------- CONVERGENCE PARAMETERS --------------------------%
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%
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CONV_CRITERIA= RESIDUAL
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CONV_FIELD= RMS_TEMPERATURE
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CONV_RESIDUAL_MINVAL= -4.07
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CONV_STARTITER= 10
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%
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% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
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%
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MESH_FILENAME= fluid_FFD.su2
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%
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SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_TEMPERATURE, STREAMWISE_MASSFLOW, STREAMWISE_DP)
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SCREEN_WRT_FREQ_INNER= 100
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%
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HISTORY_OUTPUT= ( ITER, RMS_RES, STREAMWISE_PERIODIC, FLOW_COEFF, LINSOL, AERO_COEFF )
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CONV_FILENAME= history_dptp
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%
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OUTPUT_FILES= ( RESTART, PARAVIEW_MULTIBLOCK )
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VOLUME_OUTPUT= ( COORDINATES, SOLUTION, RESIDUAL, PRIMITIVE )
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OUTPUT_WRT_FREQ= 5000
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%
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% -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
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%
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FFD_TOLERANCE= 1E-10
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FFD_ITERATIONS= 500
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%
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% FFD box definition: 2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 0.0,
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% 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0)
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FFD_DEFINITION= (BOX, 0.0029772,0.0,0.0, 0.0081772,0.0,0.0 0.0081772,0.0026,0.0, 0.0029772,0.0026,0.0, 0.0,0.0,0.0, 0.0,0.0,0.0 0.0,0.0,0.0, 0.0,0.0,0.0 )
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%
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% FFD box degree: 2D case (x_degree, y_degree, 0)
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FFD_DEGREE= (8, 1, 0)
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%
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% Surface grid continuity at the intersection with the faces of the FFD boxes.
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% To keep a particular level of surface continuity, SU2 automatically freezes the right
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% number of control point planes (NO_DERIVATIVE, 1ST_DERIVATIVE, 2ND_DERIVATIVE, USER_INPUT)
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FFD_CONTINUITY= NO_DERIVATIVE
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%
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% ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
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%
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DV_KIND= FFD_SETTING
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%DV_KIND= FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D,FFD_CONTROL_POINT_2D
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%
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% Marker of the surface in which we are going apply the shape deformation
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DV_MARKER= ( fluid_pin2_interface )
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%
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% Parameters of the shape deformation
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% - FFD_SETTING ( 1.0 )
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% - FFD_CONTROL_POINT_2D ( FFD_BoxTag, i_Ind, j_Ind, x_Disp, y_Disp )
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DV_PARAM= ( 1.0 )
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%DV_PARAM= \
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%( BOX, 0, 1, 0.0, 1.0);\
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%( BOX, 1, 1, 0.0, 1.0);\
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%( BOX, 2, 1, 0.0, 1.0);\
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%( BOX, 3, 1, 0.0, 1.0);\
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%( BOX, 4, 1, 0.0, 1.0);\
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%( BOX, 5, 1, 0.0, 1.0);\
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%( BOX, 6, 1, 0.0, 1.0);\
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%( BOX, 7, 1, 0.0, 1.0);\
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%( BOX, 8, 1, 0.0, 1.0)
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%
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% Value of the shape deformation
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DV_VALUE= 1.0
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%DV_VALUE= 1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0,1.0
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%
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% ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
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%
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DEFORM_LINEAR_SOLVER= FGMRES
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DEFORM_LINEAR_SOLVER_PREC= ILU
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DEFORM_LINEAR_SOLVER_ERROR= 1E-14
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DEFORM_NONLINEAR_ITER= 1
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DEFORM_LINEAR_SOLVER_ITER= 1000
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%
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DEFORM_CONSOLE_OUTPUT= YES
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DEFORM_STIFFNESS_TYPE= WALL_DISTANCE
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%
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% Deformation coefficient (linear elasticity limits from -1.0 to 0.5, a larger
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% value is also possible)
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% !!! What is this doing !!!
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DEFORM_COEFF = 1E6
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%
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DEFINITION_DV= \
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( 19, 1.0 | fluid_pin2_interface | BOX, 0, 1, 0.0, 1.0 ); \
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( 19, 1.0 | fluid_pin2_interface | BOX, 1, 1, 0.0, 1.0 ); \
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( 19, 1.0 | fluid_pin2_interface | BOX, 2, 1, 0.0, 1.0 ); \
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( 19, 1.0 | fluid_pin2_interface | BOX, 3, 1, 0.0, 1.0 ); \
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( 19, 1.0 | fluid_pin2_interface | BOX, 4, 1, 0.0, 1.0 ); \
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( 19, 1.0 | fluid_pin2_interface | BOX, 5, 1, 0.0, 1.0 ); \
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( 19, 1.0 | fluid_pin2_interface | BOX, 6, 1, 0.0, 1.0 ); \
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( 19, 1.0 | fluid_pin2_interface | BOX, 7, 1, 0.0, 1.0 ); \
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( 19, 1.0 | fluid_pin2_interface | BOX, 8, 1, 0.0, 1.0 )
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%DEFORM_MESH= YES
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%
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% Finite difference step size for python scripts (0.001 default, recommended
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% 0.001 x REF_LENGTH)
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FIN_DIFF_STEP= 1e-6

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