Updated configuration and MLP files for H2 burner tutorial

Author: EvertBunschoten

incompressible_flow/Inc_Combustion/1__premixed_hydrogen/H2_burner.cfg

@@ -30,10 +30,14 @@ CUSTOM_OBJFUNC= outlet_YNO
 % -------------------- FLUID MODEL --------------------------------------- %
 %
 FLUID_MODEL= FLUID_FLAMELET
+
+% List the MLP files describing the respective architectures.
 INTERPOLATION_METHOD= MLP
-FILENAMES_INTERPOLATOR= (MLP_Group1.mlp, MLP_Group2.mlp, MLP_Group3.mlp, MLP_Group4.mlp, MLP_Group5.mlp, MLP_null.mlp)
+FILENAMES_INTERPOLATOR= (MLP_TD1_n.mlp, MLP_TD2.mlp, MLP_PD.mlp, MLP_SPV.mlp, MLP_PNO.mlp, MLP_null.mlp)
+
 % FGM controlling variable names (must include mixture fraction for partial 
 % premixed cases)
+PREFERENTIAL_DIFFUSION=YES
 CONTROLLING_VARIABLE_NAMES=(ProgressVariable,EnthalpyTot,MixtureFraction)
 
 CONTROLLING_VARIABLE_SOURCE_NAMES=(ProdRateTot_PV,NULL,NULL)
@@ -65,17 +69,17 @@ SPECIES_CLIPPING= YES
 SPECIES_CLIPPING_MIN= -1.5064702033996582e+00 -3.4190245000000000e+06 +5.0012799911201000e-03   0
 SPECIES_CLIPPING_MAX= +4.6642374992370605e-01 +2.1569957500000000e+06 +1.4977467060089111e-01   1
 %
-SPECIES_INIT=(-0.5749236580085463, 2226.901776784524, 0.01446751783896619, 0)
-
-MARKER_INLET_SPECIES = (inlet, -0.5749236580085463, 2226.901776784524, 0.01446751783896619, 0)
-MARKER_INLET=(inlet, 300.0, 0.575,1,0,0)
+% Inlet and initial condition corresponding to mixture at T=300K, eq ratio 0.5
+SPECIES_INIT=(-0.575, 2.227e3, 1.447e-2, 0)
+MARKER_INLET_SPECIES = (inlet, -0.575, 2.227e3, 1.447e-29, 0)
 
 INC_INLET_TYPE= VELOCITY_INLET
+MARKER_INLET=(inlet, 300.0, 0.575,1,0,0)
 CFL_REDUCTION_SPECIES= 1.0
 
-MARKER_ISOTHERMAL=(burner_wall, 300, \
-                        cylinder_wall, 300)
-
+MARKER_ISOTHERMAL=(burner_wall, 350, \
+                        cylinder_wall, 350)
+MARKER_SPECIES_STRONG_BC=(burner_wall,cylinder_wall)
 MARKER_INTERNAL=(fluid)
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 %
@@ -100,7 +104,7 @@ MARKER_OUTLET= (outlet, 0.0)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 150
 CFL_ADAPT= NO
-ITER= 1000
+ITER= 3000
 %
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
@@ -116,7 +120,7 @@ MGLEVEL= 0
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= FDS
-MUSCL_FLOW= NO
+MUSCL_FLOW= YES
 SLOPE_LIMITER_FLOW = NONE
 TIME_DISCRE_FLOW= EULER_IMPLICIT
 %
@@ -126,18 +130,15 @@ CONV_RESIDUAL_MINVAL= -15
 CONV_STARTITER= 10
 CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
-SCREEN_OUTPUT = INNER_ITER RMS_VELOCITY-X RMS_PRESSURE RMS_ProgressVariable RMS_EnthalpyTot RMS_MixtureFraction CUSTOM
-%__ADJOINT__SCREEN_OUTPUT = INNER_ITER RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_PRESSURE RMS_ADJ_ProgressVariable RMS_ADJ_EnthalpyTot RMS_ADJ_MixtureFraction
-HISTORY_OUTPUT = RMS_RES CUSTOM
-%__ADJOINT__HISTORY_OUTPUT = RMS_RES
+SCREEN_OUTPUT = INNER_ITER RMS_VELOCITY-X RMS_PRESSURE RMS_ProgressVariable RMS_EnthalpyTot RMS_MixtureFraction
+HISTORY_OUTPUT = RMS_RES 
 VOLUME_OUTPUT = SOLUTION RESIDUAL SENSITIVITY LOOKUP TIMESTEP PRIMITIVE SOURCE
 CONV_FIELD = RMS_PRESSURE, RMS_VELOCITY-Z, RMS_VELOCITY-Y, RMS_MixtureFraction
-%__ADJOINT__CONV_FIELD = RMS_ADJ_PRESSURE, RMS_ADJ_VELOCITY-X, RMS_ADJ_VELOCITY-Y, RMS_ADJ_MixtureFraction
 WRT_ZONE_HIST= YES
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-RESTART_SOL=YES
+RESTART_SOL=NO
 OUTPUT_PRECISION= 16
 TABULAR_FORMAT = CSV
 MESH_FILENAME=H2_burner.su2