Merge pull request #74 from su2code/develop

pcarruscag · web-flow · commit 28aaa49e08ec · 2026-01-11T16:14:24.000-08:00
Develop
diff --git a/design/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg b/design/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg
@@ -78,7 +78,7 @@ MARKER_OUTLET= ( outlet, 10000.0 )
 MARKER_PLOTTING= ( lower )
 %
 % Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
-MARKER_MONITORING= (outlet, lower)
+MARKER_MONITORING= ( lower )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
@@ -274,6 +274,8 @@ READ_BINARY_RESTART = NO
 % Screen output
 SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)
 %
+HISTORY_OUTPUT= (INNER_ITER, RMS_RES, AERO_COEFF, COMBO)
+%
 OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW, SURFACE_CSV)
 
 % -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%
diff --git a/incompressible_flow/Inc_Combustion/1__premixed_hydrogen/H2_burner.cfg b/incompressible_flow/Inc_Combustion/1__premixed_hydrogen/H2_burner.cfg
@@ -55,7 +55,8 @@ DIFFUSIVITY_MODEL= FLAMELET
 VISCOSITY_MODEL= FLAMELET
 CONDUCTIVITY_MODEL= FLAMELET
 
-FLAME_INIT_METHOD= SPARK
+%FLAME_INIT_METHOD= SPARK
+FLAME_INIT_METHOD= NONE 
 SPARK_INIT= (0.001, 0.0004, 0.00, 1e-4, 100, 5)
 SPARK_REACTION_RATES=(1000, 0, 0)
 
@@ -101,9 +102,9 @@ MARKER_OUTLET= (outlet, 0.0)
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
-CFL_NUMBER= 150
+CFL_NUMBER= 50
 CFL_ADAPT= NO
-ITER= 5
+ITER= 5000
 %
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
@@ -131,14 +132,14 @@ CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
 SCREEN_OUTPUT = INNER_ITER RMS_VELOCITY-X RMS_PRESSURE RMS_ProgressVariable RMS_EnthalpyTot RMS_MixtureFraction
 HISTORY_OUTPUT = RMS_RES 
-VOLUME_OUTPUT = SOLUTION
+VOLUME_OUTPUT = SOLUTION, RESIDUAL, PRIMITIVE
 CONV_FIELD = RMS_PRESSURE, RMS_VELOCITY-Z, RMS_VELOCITY-Y, RMS_MixtureFraction
 WRT_ZONE_HIST= YES
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
-RESTART_SOL=YES
+RESTART_SOL= YES
 OUTPUT_PRECISION= 16
 TABULAR_FORMAT = CSV
 MESH_FILENAME=H2_burner.su2
-OUTPUT_FILES=(RESTART, PARAVIEW_MULTIBLOCK)
+OUTPUT_FILES=(RESTART, PARAVIEW_MULTIBLOCK)
diff --git a/incompressible_flow/Inc_Combustion/1__premixed_hydrogen/solution.dat b/incompressible_flow/Inc_Combustion/1__premixed_hydrogen/solution.dat
diff --git a/incompressible_flow/Inc_Laminar_Cavity/lam_buoyancy_cavity.cfg b/incompressible_flow/Inc_Laminar_Cavity/lam_buoyancy_cavity.cfg
@@ -198,7 +198,7 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
 % Convergence criteria (CAUCHY, RESIDUAL)
-CONV_FIELD= RMS_TEMPERATURE
+CONV_FIELD= RMS_ENTHALPY
 %
 % Min value of the residual (log10 of the residual)
 CONV_RESIDUAL_MINVAL= -8
@@ -261,4 +261,4 @@ OUTPUT_WRT_FREQ= 100
 %
 %
 % Screen output
-SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_TEMPERATURE, LIFT, DRAG)
+SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_ENTHALPY, LIFT, DRAG)
diff --git a/incompressible_flow/Inc_Species_Transport/solution.csv b/incompressible_flow/Inc_Species_Transport/solution.csv
diff --git a/incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_dp_hf_tp.cfg b/incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_dp_hf_tp.cfg
@@ -103,15 +103,15 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-CONV_FIELD= RMS_TEMPERATURE
+CONV_FIELD= RMS_ENTHALPY
 CONV_RESIDUAL_MINVAL= -4.07
 CONV_STARTITER= 10
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= fluid_FFD.su2
 %
-SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_TEMPERATURE, STREAMWISE_MASSFLOW, STREAMWISE_DP)
+SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_ENTHALPY, STREAMWISE_MASSFLOW, STREAMWISE_DP)
 SCREEN_WRT_FREQ_INNER= 100
 %
 HISTORY_OUTPUT= ( ITER, RMS_RES, STREAMWISE_PERIODIC, FLOW_COEFF, LINSOL, AERO_COEFF )
diff --git a/incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_mf_hf.cfg b/incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_mf_hf.cfg
@@ -108,15 +108,15 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %
-CONV_FIELD= RMS_TEMPERATURE
+CONV_FIELD= RMS_ENTHALPY
 CONV_RESIDUAL_MINVAL= -10.9
 CONV_STARTITER= 10
 %
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= fluid_FFD.su2
 %
-SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_TEMPERATURE, STREAMWISE_MASSFLOW, STREAMWISE_DP)
+SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_ENTHALPY, STREAMWISE_MASSFLOW, STREAMWISE_DP)
 SCREEN_WRT_FREQ_INNER= 100
 %
 HISTORY_OUTPUT= ( ITER, RMS_RES, STREAMWISE_PERIODIC, FLOW_COEFF, LINSOL, AERO_COEFF )
diff --git a/multiphysics/unsteady_cht/cht_2d_3cylinders.cfg b/multiphysics/unsteady_cht/cht_2d_3cylinders.cfg
@@ -33,7 +33,7 @@ CFL_NUMBER= 100.0
 MESH_FILENAME= mesh_cht_3cyl.su2
 %
 SCREEN_OUTPUT= ( TIME_ITER, OUTER_ITER, \
- BGS_PRESSURE[0], BGS_TEMPERATURE[0], BGS_TEMPERATURE[1], BGS_TEMPERATURE[2], BGS_TEMPERATURE[3], \
+ BGS_PRESSURE[0], BGS_ENTHALPY[0], BGS_TEMPERATURE[1], BGS_TEMPERATURE[2], BGS_TEMPERATURE[3], \
  DRAG[0], SURFACE_STATIC_TEMPERATURE[0], AVG_TEMPERATURE[1], TOTAL_HEATFLUX[1] )
 SCREEN_WRT_FREQ_OUTER= 25
 %

Original file line number	Diff line number	Diff line change
`@@ -78,7 +78,7 @@ MARKER_OUTLET= ( outlet, 10000.0 )`
`78`	`78`	`MARKER_PLOTTING= ( lower )`
`79`	`79`	`%`
`80`	`80`	`% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated`
`81`		`-MARKER_MONITORING= (outlet, lower)`
	`81`	`+MARKER_MONITORING= ( lower )`
`82`	`82`
`83`	`83`	`% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%`
`84`	`84`	`%`
`@@ -274,6 +274,8 @@ READ_BINARY_RESTART = NO`
`274`	`274`	`% Screen output`
`275`	`275`	`SCREEN_OUTPUT= (INNER_ITER, RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, SENS_GEO, SENS_AOA)`
`276`	`276`	`%`
	`277`	`+HISTORY_OUTPUT= (INNER_ITER, RMS_RES, AERO_COEFF, COMBO)`
	`278`	`+%`
`277`	`279`	`OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW, SURFACE_CSV)`
`278`	`280`
`279`	`281`	`% -------------------- FREE-FORM DEFORMATION PARAMETERS -----------------------%`
Original file line number	Diff line number	Diff line change
`@@ -198,7 +198,7 @@ TIME_DISCRE_FLOW= EULER_IMPLICIT`
`198`	`198`	`% --------------------------- CONVERGENCE PARAMETERS --------------------------%`
`199`	`199`	`%`
`200`	`200`	`% Convergence criteria (CAUCHY, RESIDUAL)`
`201`		`-CONV_FIELD= RMS_TEMPERATURE`
	`201`	`+CONV_FIELD= RMS_ENTHALPY`
`202`	`202`	`%`
`203`	`203`	`% Min value of the residual (log10 of the residual)`
`204`	`204`	`CONV_RESIDUAL_MINVAL= -8`
`@@ -261,4 +261,4 @@ OUTPUT_WRT_FREQ= 100`
`261`	`261`	`%`
`262`	`262`	`%`
`263`	`263`	`% Screen output`
`264`		`-SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_TEMPERATURE, LIFT, DRAG)`
	`264`	`+SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_ENTHALPY, LIFT, DRAG)`
Original file line number	Diff line number	Diff line change
`@@ -103,15 +103,15 @@ TIME_DISCRE_TURB= EULER_IMPLICIT`
`103`	`103`	`%`
`104`	`104`	`% --------------------------- CONVERGENCE PARAMETERS --------------------------%`
`105`	`105`	`%`
`106`		`-CONV_FIELD= RMS_TEMPERATURE`
	`106`	`+CONV_FIELD= RMS_ENTHALPY`
`107`	`107`	`CONV_RESIDUAL_MINVAL= -4.07`
`108`	`108`	`CONV_STARTITER= 10`
`109`	`109`	`%`
`110`	`110`	`% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%`
`111`	`111`	`%`
`112`	`112`	`MESH_FILENAME= fluid_FFD.su2`
`113`	`113`	`%`
`114`		`-SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_TEMPERATURE, STREAMWISE_MASSFLOW, STREAMWISE_DP)`
	`114`	`+SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_ENTHALPY, STREAMWISE_MASSFLOW, STREAMWISE_DP)`
`115`	`115`	`SCREEN_WRT_FREQ_INNER= 100`
`116`	`116`	`%`
`117`	`117`	`HISTORY_OUTPUT= ( ITER, RMS_RES, STREAMWISE_PERIODIC, FLOW_COEFF, LINSOL, AERO_COEFF )`
Original file line number	Diff line number	Diff line change
`@@ -108,15 +108,15 @@ TIME_DISCRE_TURB= EULER_IMPLICIT`
`108`	`108`	`%`
`109`	`109`	`% --------------------------- CONVERGENCE PARAMETERS --------------------------%`
`110`	`110`	`%`
`111`		`-CONV_FIELD= RMS_TEMPERATURE`
	`111`	`+CONV_FIELD= RMS_ENTHALPY`
`112`	`112`	`CONV_RESIDUAL_MINVAL= -10.9`
`113`	`113`	`CONV_STARTITER= 10`
`114`	`114`	`%`
`115`	`115`	`% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%`
`116`	`116`	`%`
`117`	`117`	`MESH_FILENAME= fluid_FFD.su2`
`118`	`118`	`%`
`119`		`-SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_TEMPERATURE, STREAMWISE_MASSFLOW, STREAMWISE_DP)`
	`119`	`+SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_ENTHALPY, STREAMWISE_MASSFLOW, STREAMWISE_DP)`
`120`	`120`	`SCREEN_WRT_FREQ_INNER= 100`
`121`	`121`	`%`
`122`	`122`	`HISTORY_OUTPUT= ( ITER, RMS_RES, STREAMWISE_PERIODIC, FLOW_COEFF, LINSOL, AERO_COEFF )`
Original file line number	Diff line number	Diff line change
`@@ -33,7 +33,7 @@ CFL_NUMBER= 100.0`
`33`	`33`	`MESH_FILENAME= mesh_cht_3cyl.su2`
`34`	`34`	`%`
`35`	`35`	`SCREEN_OUTPUT= ( TIME_ITER, OUTER_ITER, \`
`36`		`- BGS_PRESSURE[0], BGS_TEMPERATURE[0], BGS_TEMPERATURE[1], BGS_TEMPERATURE[2], BGS_TEMPERATURE[3], \`
	`36`	`+ BGS_PRESSURE[0], BGS_ENTHALPY[0], BGS_TEMPERATURE[1], BGS_TEMPERATURE[2], BGS_TEMPERATURE[3], \`
`37`	`37`	`DRAG[0], SURFACE_STATIC_TEMPERATURE[0], AVG_TEMPERATURE[1], TOTAL_HEATFLUX[1] )`
`38`	`38`	`SCREEN_WRT_FREQ_OUTER= 25`
`39`	`39`	`%`