Merge pull request #42 from su2code/feature_new_flamelet

bigfooted · web-flow · commit 12b593e95113 · 2023-06-07T13:43:49.000+02:00
remove USE_SPECIES_STRONG_BC
diff --git a/incompressible_flow/Inc_Species_Transport/1__FFD-box-writing/species3_primitiveVenturi.cfg b/incompressible_flow/Inc_Species_Transport/1__FFD-box-writing/species3_primitiveVenturi.cfg
@@ -50,7 +50,7 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
+
 MARKER_INLET_SPECIES= (gas_inlet,       0.5, 0.5,\
                        air_axial_inlet, 0.6, 0.0 )
 %
diff --git a/incompressible_flow/Inc_Species_Transport/2__mesh-deform-test/species3_primitiveVenturi_deform.cfg b/incompressible_flow/Inc_Species_Transport/2__mesh-deform-test/species3_primitiveVenturi_deform.cfg
@@ -51,7 +51,7 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
+
 MARKER_INLET_SPECIES= (gas_inlet,       0.5, 0.5,\
                        air_axial_inlet, 0.6, 0.0 )
 %
diff --git a/incompressible_flow/Inc_Species_Transport/3__gradient-validation/species3_primitiveVenturi.cfg b/incompressible_flow/Inc_Species_Transport/3__gradient-validation/species3_primitiveVenturi.cfg
@@ -54,7 +54,7 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
+
 MARKER_INLET_SPECIES= (gas_inlet,       0.5, 0.5,\
                        air_axial_inlet, 0.6, 0.0 )
 %
diff --git a/incompressible_flow/Inc_Species_Transport/4__optimization/species3_primitiveVenturi.cfg b/incompressible_flow/Inc_Species_Transport/4__optimization/species3_primitiveVenturi.cfg
@@ -54,7 +54,7 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
+
 MARKER_INLET_SPECIES= (gas_inlet,       0.5, 0.5,\
                        air_axial_inlet, 0.6, 0.0 )
 %
diff --git a/incompressible_flow/Inc_Species_Transport/DAspecies3_primitiveVenturi.cfg b/incompressible_flow/Inc_Species_Transport/DAspecies3_primitiveVenturi.cfg
@@ -58,7 +58,7 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
+
 MARKER_INLET_SPECIES= (gas_inlet,       0.5, 0.5,\
                        air_axial_inlet, 0.6, 0.0 )
 %
diff --git a/incompressible_flow/Inc_Species_Transport/species3_primitiveVenturi.cfg b/incompressible_flow/Inc_Species_Transport/species3_primitiveVenturi.cfg
@@ -50,7 +50,7 @@ INLET_FILENAME= inlet_venturi.dat
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( gas_inlet,       300, 1.0, 1.0,  0.0, 0.0,\
                 air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
-SPECIES_USE_STRONG_BC= NO
+
 MARKER_INLET_SPECIES= (gas_inlet,       0.5, 0.5,\
                        air_axial_inlet, 0.6, 0.0 )
 %
diff --git a/incompressible_flow/Inc_Species_Transport_Composition_Dependent_Model/kenics_mixer_tutorial.cfg b/incompressible_flow/Inc_Species_Transport_Composition_Dependent_Model/kenics_mixer_tutorial.cfg
@@ -60,7 +60,7 @@ SPECIFIED_INLET_PROFILE= NO
 %
 INC_INLET_TYPE=  VELOCITY_INLET VELOCITY_INLET
 MARKER_INLET= ( inlet_gas, 300, 5.0, 0.0,  0.0, 1.0, inlet_air, 300, 5.0, 0.0, 0.0, 1.0 )
-SPECIES_USE_STRONG_BC= NO
+
 MARKER_INLET_SPECIES= ( inlet_gas, 1.0, inlet_air, 0.0 )
 %
 MARKER_INLET_TURBULENT= ( inlet_gas, 0.05, 10, inlet_air, 0.05, 10 )

Original file line number	Diff line number	Diff line change
`@@ -50,7 +50,7 @@ INLET_FILENAME= inlet_venturi.dat`
`50`	`50`	`INC_INLET_TYPE= VELOCITY_INLET VELOCITY_INLET`
`51`	`51`	`MARKER_INLET= ( gas_inlet, 300, 1.0, 1.0, 0.0, 0.0,\`
`52`	`52`	`air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )`
`53`		`-SPECIES_USE_STRONG_BC= NO`
	`53`	`+`
`54`	`54`	`MARKER_INLET_SPECIES= (gas_inlet, 0.5, 0.5,\`
`55`	`55`	`air_axial_inlet, 0.6, 0.0 )`
`56`	`56`	`%`
Original file line number	Diff line number	Diff line change
`@@ -51,7 +51,7 @@ INLET_FILENAME= inlet_venturi.dat`
`51`	`51`	`INC_INLET_TYPE= VELOCITY_INLET VELOCITY_INLET`
`52`	`52`	`MARKER_INLET= ( gas_inlet, 300, 1.0, 1.0, 0.0, 0.0,\`
`53`	`53`	`air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )`
`54`		`-SPECIES_USE_STRONG_BC= NO`
	`54`	`+`
`55`	`55`	`MARKER_INLET_SPECIES= (gas_inlet, 0.5, 0.5,\`
`56`	`56`	`air_axial_inlet, 0.6, 0.0 )`
`57`	`57`	`%`
Original file line number	Diff line number	Diff line change
`@@ -54,7 +54,7 @@ INLET_FILENAME= inlet_venturi.dat`
`54`	`54`	`INC_INLET_TYPE= VELOCITY_INLET VELOCITY_INLET`
`55`	`55`	`MARKER_INLET= ( gas_inlet, 300, 1.0, 1.0, 0.0, 0.0,\`
`56`	`56`	`air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )`
`57`		`-SPECIES_USE_STRONG_BC= NO`
	`57`	`+`
`58`	`58`	`MARKER_INLET_SPECIES= (gas_inlet, 0.5, 0.5,\`
`59`	`59`	`air_axial_inlet, 0.6, 0.0 )`
`60`	`60`	`%`
Original file line number	Diff line number	Diff line change
`@@ -58,7 +58,7 @@ INLET_FILENAME= inlet_venturi.dat`
`58`	`58`	`INC_INLET_TYPE= VELOCITY_INLET VELOCITY_INLET`
`59`	`59`	`MARKER_INLET= ( gas_inlet, 300, 1.0, 1.0, 0.0, 0.0,\`
`60`	`60`	`air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )`
`61`		`-SPECIES_USE_STRONG_BC= NO`
	`61`	`+`
`62`	`62`	`MARKER_INLET_SPECIES= (gas_inlet, 0.5, 0.5,\`
`63`	`63`	`air_axial_inlet, 0.6, 0.0 )`
`64`	`64`	`%`
Original file line number	Diff line number	Diff line change
`@@ -60,7 +60,7 @@ SPECIFIED_INLET_PROFILE= NO`
`60`	`60`	`%`
`61`	`61`	`INC_INLET_TYPE= VELOCITY_INLET VELOCITY_INLET`
`62`	`62`	`MARKER_INLET= ( inlet_gas, 300, 5.0, 0.0, 0.0, 1.0, inlet_air, 300, 5.0, 0.0, 0.0, 1.0 )`
`63`		`-SPECIES_USE_STRONG_BC= NO`
	`63`	`+`
`64`	`64`	`MARKER_INLET_SPECIES= ( inlet_gas, 1.0, inlet_air, 0.0 )`
`65`	`65`	`%`
`66`	`66`	`MARKER_INLET_TURBULENT= ( inlet_gas, 0.05, 10, inlet_air, 0.05, 10 )`