Merge pull request #16 from su2code/feature_heatcoeff_BC

Feature heatcoeff bc

Author: TobiKattmann

compressible_flow/NICFD_nozzle/NICFD_nozzle.cfg

@@ -104,7 +104,7 @@ MU_CONSTANT= 1.21409E-05
 CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
 %
 % Molecular Thermal Conductivity that would be constant (0.0257 by default)
-KT_CONSTANT= 0.030542828
+THERMAL_CONDUCTIVITY_CONSTANT= 0.030542828
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %

incompressible_flow/Inc_Laminar_Cavity/lam_buoyancy_cavity.cfg

@@ -77,7 +77,7 @@ MU_CONSTANT= 1.716e-5
 CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
 %
 % Molecular Thermal Conductivity that would be constant (0.0257 by default)
-KT_CONSTANT= 0.0246295028571
+THERMAL_CONDUCTIVITY_CONSTANT= 0.0246295028571
 
 % ----------------------- BODY FORCE DEFINITION -------------------------------%
 %

multiphysics/steady_cht/cht_2d_3cylinders.cfg

@@ -5,10 +5,9 @@
 % Author: O. Burghardt, T. Economon                                             %
 % Institution: Chair for Scientific Computing, TU Kaiserslautern                %
 % Date: August 8, 2019                                                          %
-% File Version 6.0.1 "Falcon"                                                   %
+% File Version 7.1.1 "Blackbird"                                                %
 %                                                                               %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
 %
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
@@ -18,67 +17,34 @@ SOLVER= MULTIPHYSICS
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
 %
-% Restart solution (NO, YES)
-RESTART_SOL= NO
 %
-% Configuration file list, one for each physical zone 
-CONFIG_LIST= (flow_cylinder.cfg, solid_cylinder1.cfg, solid_cylinder2.cfg, solid_cylinder3.cfg)
+CONFIG_LIST = (flow_cylinder.cfg, solid_cylinder1.cfg, solid_cylinder2.cfg, solid_cylinder3.cfg)
+%
 %
-% Definition of the interface
 MARKER_ZONE_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
+%
+%
 MARKER_CHT_INTERFACE= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
 %
-% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
-%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
-%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
-%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
-%                                             TORQUE, TOTAL_HEATFLUX,
-%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
-%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
-%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
-% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
-OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
 %
-% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
-OBJECTIVE_WEIGHT= 1.0
+CHT_COUPLING_METHOD= DIRECT_TEMPERATURE_ROBIN_HEATFLUX
+%
+%
+TIME_DOMAIN = NO
 %
-% Number of total iterations
-OUTER_ITER = 15000
-OUTPUT_WRT_FREQ = 15000
+% Number of total iterations (15000 for suitable results)
+OUTER_ITER = 11
 %
 % Mesh input file
 MESH_FILENAME= mesh_cht_3cyl_ffd.su2
-MESH_OUT_FILENAME= mesh_cht_3cyl_out.su2
 %
 % Mesh input file format (SU2, CGNS, NETCDF_ASCII)
 MESH_FORMAT= SU2
 %
 % Output file format
-OUTPUT_FILES= (RESTART, TECPLOT, PARAVIEW, SURFACE_TECPLOT, SURFACE_PARAVIEW)
-%
-% Multizone convergence criteria
-CONV_RESIDUAL_MINVAL= -20
-
-% -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
-%
-% Tolerance of the Free-Form Deformation point inversion
-FFD_TOLERANCE= 1E-12
-%
-% Maximum number of iterations in the Free-Form Deformation point inversion
-FFD_ITERATIONS= 500
-%
-% FFD box definition: 3D case (FFD_BoxTag, X1, Y1, Z1, X2, Y2, Z2, X3, Y3, Z3, X4, Y4, Z4,
-%                              X5, Y5, Z5, X6, Y6, Z6, X7, Y7, Z7, X8, Y8, Z8)
-%                     2D case (FFD_BoxTag, X1, Y1, 0.0, X2, Y2, 0.0, X3, Y3, 0.0, X4, Y4, 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)
-FFD_DEFINITION= (MAIN_BOX, -0.1, -0.6, 0.0, 1.1, -0.6, 0.0, 1.1, 0.6, 0.0, -0.1, 0.6, 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)
-%
-% FFD box degree: 3D case (x_degree, y_degree, z_degree)
-%                 2D case (x_degree, y_degree, 0)
-FFD_DEGREE= ( 24, 1, 0)
+OUTPUT_FILES= (RESTART, PARAVIEW_MULTIBLOCK)
 %
-% Surface continuity at the intersection with the FFD (1ST_DERIVATIVE, 2ND_DERIVATIVE)
-FFD_CONTINUITY= 2ND_DERIVATIVE
+% These are just default parameters so that we can run SU2_DOT_AD, they have no physical meaning for this test case.
 
 % ----------------------- DESIGN VARIABLE PARAMETERS --------------------------%
 %
@@ -87,10 +53,10 @@ FFD_CONTINUITY= 2ND_DERIVATIVE
 %                      FFD_CONTROL_POINT, FFD_CAMBER, FFD_THICKNESS, FFD_TWIST
 %                      FFD_CONTROL_POINT_2D, FFD_CAMBER_2D, FFD_THICKNESS_2D, FFD_TWIST_2D,
 %                      HICKS_HENNE, SURFACE_BUMP)
-DV_KIND= FFD_CONTROL_POINT_2D
+DV_KIND= HICKS_HENNE
 %
 % Marker of the surface in which we are going apply the shape deformation
-DV_MARKER= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3)
+DV_MARKER= ( cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2, cylinder_outer3, cylinder_inner3  )
 %
 % Parameters of the shape deformation
 % - NO_DEFORMATION ( 1.0 )
@@ -112,7 +78,7 @@ DV_MARKER= (cylinder_outer1, cylinder_inner1, cylinder_outer2, cylinder_inner2,
 % - FFD_TWIST_2D ( FFD_BoxTag, x_Orig, y_Orig )
 % - HICKS_HENNE ( Lower Surface (0)/Upper Surface (1)/Only one Surface (2), x_Loc )
 % - SURFACE_BUMP ( x_Start, x_End, x_Loc )
-DV_PARAM= ( MAIN_BOX, 12, 1, 0.0, 1.0 )
+DV_PARAM= (0.0, 0.5)
 %
 % Value of the shape deformation
 DV_VALUE= 0.1

multiphysics/steady_cht/flow_cylinder.cfg

@@ -15,20 +15,28 @@ SOLVER= INC_NAVIER_STOKES
 % If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= NONE
 %
-% Data written to history file
-WRT_ZONE_HIST= YES
-HISTORY_OUTPUT= (ITER, RMS_RES, HEAT)
-%
-% Number of inner iteration
-INNER_ITER=1
-
-% --------------------------- CONVERGENCE PARAMETERS --------------------------%
-%
-% Min value of the residual (log10 of the residual)
-CONV_RESIDUAL_MINVAL= -20
+% Restart solution (NO, YES)
+RESTART_SOL= NO
+%
+% Objective function in gradient evaluation   (DRAG, LIFT, SIDEFORCE, MOMENT_X,
+%                                             MOMENT_Y, MOMENT_Z, EFFICIENCY,
+%                                             EQUIVALENT_AREA, NEARFIELD_PRESSURE,
+%                                             FORCE_X, FORCE_Y, FORCE_Z, THRUST,
+%                                             TORQUE, TOTAL_HEATFLUX,
+%                                             MAXIMUM_HEATFLUX, INVERSE_DESIGN_PRESSURE,
+%                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
+%                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
+% For a weighted sum of objectives: separate by commas, add OBJECTIVE_WEIGHT and MARKER_MONITORING in matching order.
+OBJECTIVE_FUNCTION= TOTAL_HEATFLUX
+%
+% List of weighting values when using more than one OBJECTIVE_FUNCTION. Separate by commas and match with MARKER_MONITORING.
+OBJECTIVE_WEIGHT = 1.0
+%
+% Read binary restart files (YES, NO)
+READ_BINARY_RESTART = YES
 %
-% Start convergence criteria at iteration number
-CONV_STARTITER= 0
+% Data written to history file
+HISTORY_OUTPUT=(ITER, RMS_RES, HEAT )
 
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
 %
@@ -52,7 +60,7 @@ INC_DENSITY_MODEL= VARIABLE
 INC_ENERGY_EQUATION = YES
 %
 % Initial density for incompressible flows (1.2886 kg/m^3 by default)
-INC_DENSITY_INIT= 0.00042
+INC_DENSITY_INIT= 0.000210322
 %
 % Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 3.40297, 0.0, 0.0 )
@@ -104,7 +112,7 @@ SUTHERLAND_CONSTANT= 110.4
 CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
 %
 % Molecular Thermal Conductivity that would be constant (0.0257 by default)
-KT_CONSTANT= 0.0257
+THERMAL_CONDUCTIVITY_CONSTANT= 0.0257
 %
 % Laminar Prandtl number (0.72 (air), only for CONSTANT_PRANDTL)
 PRANDTL_LAM= 0.72
@@ -118,7 +126,7 @@ PRANDTL_TURB= 0.90
 NUM_METHOD_GRAD= GREEN_GAUSS
 %
 % Courant-Friedrichs-Lewy condition of the finest grid
-CFL_NUMBER= 50.0
+CFL_NUMBER= 10.0
 %
 % Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
@@ -140,14 +148,14 @@ LINEAR_SOLVER= FGMRES
 % Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI)
 LINEAR_SOLVER_PREC= ILU
 %
-% Linael solver ILU preconditioner fill-in level (0 by default)
+% Linear solver ILU preconditioner fill-in level (0 by default)
 LINEAR_SOLVER_ILU_FILL_IN= 0
 %
 % Minimum error of the linear solver for implicit formulations
 LINEAR_SOLVER_ERROR= 1E-15
 %
 % Max number of iterations of the linear solver for the implicit formulation
-LINEAR_SOLVER_ITER= 10
+LINEAR_SOLVER_ITER= 5
 
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
@@ -166,34 +174,19 @@ SLOPE_LIMITER_FLOW= NONE
 % Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 
-% ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
-VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the adjoint sharp edges limiter (3.0 by default).
-ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Freeze the value of the limiter after a number of iterations
-LIMITER_ITER= 999999
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-% 1st order artificial dissipation coefficients for
-%     the Lax–Friedrichs method ( 0.15 by default )
-LAX_SENSOR_COEFF= 0.15
+% Min value of the residual (log10 of the residual)
+CONV_RESIDUAL_MINVAL= -19
 %
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
-JST_SENSOR_COEFF= ( 0.5, 0.05 )
+% Start convergence criteria at iteration number
+CONV_STARTITER= 10
 %
-% 1st order artificial dissipation coefficients for
-%     the adjoint Lax–Friedrichs method ( 0.15 by default )
-ADJ_LAX_SENSOR_COEFF= 0.15
+% Number of elements to apply the criteria
+CONV_CAUCHY_ELEMS= 100
 %
-% 2nd, and 4th order artificial dissipation coefficients for
-%     the adjoint JST method ( 0.5, 0.02 by default )
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
+% Epsilon to control the series convergence
+CONV_CAUCHY_EPS= 1E-6
 
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
@@ -203,6 +196,10 @@ SOLUTION_FILENAME= solution_flow.dat
 % Restart adjoint input file
 SOLUTION_ADJ_FILENAME= solution_adj.dat
 %
+% Output file format (TECPLOT, TECPLOT_BINARY, PARAVIEW,
+%                     FIELDVIEW, FIELDVIEW_BINARY)
+TABULAR_FORMAT= TECPLOT
+%
 % Output file convergence history (w/o extension)
 CONV_FILENAME= history
 %
@@ -232,3 +229,23 @@ SURFACE_FILENAME= surface_flow
 %
 % Output file surface adjoint coefficient (w/o extension)
 SURFACE_ADJ_FILENAME= surface_adjoint
+%
+
+% ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
+%
+% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
+DEFORM_LINEAR_SOLVER= FGMRES
+%
+% Number of smoothing iterations for mesh deformation
+DEFORM_LINEAR_SOLVER_ITER= 200
+%
+% Number of nonlinear deformation iterations (surface deformation increments)
+DEFORM_NONLINEAR_ITER= 1
+%
+% Print the residuals during mesh deformation to the console (YES, NO)
+DEFORM_CONSOLE_OUTPUT= YES
+%
+% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
+%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
+DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
+