update air_nozzle regression

WallyMaier · WallyMaier · commit a28c38db6559 · 2022-07-07T08:18:42.000-07:00
diff --git a/TestCases/axisymmetric_rans/air_nozzle/air_nozzle.cfg b/TestCases/axisymmetric_rans/air_nozzle/air_nozzle.cfg
@@ -54,10 +54,10 @@ MARKER_MONITORING = (WALL)
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
 NUM_METHOD_GRAD= GREEN_GAUSS
-%
 CFL_NUMBER= 1000.0
 CFL_ADAPT= NO
 MAX_DELTA_TIME= 1E6
+OBJECTIVE_FUNCTION= DRAG
 %
 % ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
 %
@@ -72,10 +72,6 @@ LINEAR_SOLVER_ILU_FILL_IN= 0
 LINEAR_SOLVER_ERROR= 0.01
 LINEAR_SOLVER_ITER= 10
 %
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-MGLEVEL= 0
-%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 CONV_NUM_METHOD_FLOW= ROE
@@ -103,4 +99,4 @@ OUTPUT_WRT_FREQ= 1000
 %
 % Note: This cfg is used for a primal and adjoint Testcase, therefore both residuals are present here.
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, RMS_TKE, RMS_DISSIPATION, TOTAL_HEATFLUX, \
-                RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION)
+                RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION, SENS_AOA, SENS_MACH)

Original file line number	Diff line number	Diff line change
`@@ -54,10 +54,10 @@ MARKER_MONITORING = (WALL)`
`54`	`54`	`% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%`
`55`	`55`	`%`
`56`	`56`	`NUM_METHOD_GRAD= GREEN_GAUSS`
`57`		`-%`
`58`	`57`	`CFL_NUMBER= 1000.0`
`59`	`58`	`CFL_ADAPT= NO`
`60`	`59`	`MAX_DELTA_TIME= 1E6`
	`60`	`+OBJECTIVE_FUNCTION= DRAG`
`61`	`61`	`%`
`62`	`62`	`% ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%`
`63`	`63`	`%`
`@@ -72,10 +72,6 @@ LINEAR_SOLVER_ILU_FILL_IN= 0`
`72`	`72`	`LINEAR_SOLVER_ERROR= 0.01`
`73`	`73`	`LINEAR_SOLVER_ITER= 10`
`74`	`74`	`%`
`75`		`-% -------------------------- MULTIGRID PARAMETERS -----------------------------%`
`76`		`-%`
`77`		`-MGLEVEL= 0`
`78`		`-%`
`79`	`75`	`% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%`
`80`	`76`	`%`
`81`	`77`	`CONV_NUM_METHOD_FLOW= ROE`
`@@ -103,4 +99,4 @@ OUTPUT_WRT_FREQ= 1000`
`103`	`99`	`%`
`104`	`100`	`% Note: This cfg is used for a primal and adjoint Testcase, therefore both residuals are present here.`
`105`	`101`	`SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_ENERGY, RMS_TKE, RMS_DISSIPATION, TOTAL_HEATFLUX, \`
`106`		`- RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION)`
	`102`	`+ RMS_ADJ_DENSITY, RMS_ADJ_ENERGY, RMS_ADJ_TKE, RMS_ADJ_DISSIPATION, SENS_AOA, SENS_MACH)`