Two fixes for tutorial regressions.

economon · economon · commit ceaeacc9eefe · 2019-11-26T08:21:44.000-08:00
diff --git a/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg b/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg
@@ -90,7 +90,7 @@ NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 CFL_NUMBER= 1.0
 %
 % Adaptive CFL number (NO, YES)
-CFL_ADAPT= YES
+CFL_ADAPT= NO
 %
 % Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
 %                                        CFL max value )
diff --git a/Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg b/Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg
@@ -177,9 +177,6 @@ ENTROPY_FIX_COEFF= 0.001
 %
 % Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
 TIME_DISCRE_FLOW= EULER_IMPLICIT
-%
-% Relaxation coefficient
-RELAXATION_FACTOR_FLOW= 0.95
 
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
 %
@@ -191,9 +188,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT
 %
 % Reduction factor of the CFL coefficient in the turbulence problem
 CFL_REDUCTION_TURB= 1.0
-%
-% Relaxation coefficient
-RELAXATION_FACTOR_TURB= 0.95
 
 % ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%
 %

Original file line number	Diff line number	Diff line change
`@@ -90,7 +90,7 @@ NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES`
`90`	`90`	`CFL_NUMBER= 1.0`
`91`	`91`	`%`
`92`	`92`	`% Adaptive CFL number (NO, YES)`
`93`		`-CFL_ADAPT= YES`
	`93`	`+CFL_ADAPT= NO`
`94`	`94`	`%`
`95`	`95`	`% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,`
`96`	`96`	`% CFL max value )`
Original file line number	Diff line number	Diff line change
`@@ -177,9 +177,6 @@ ENTROPY_FIX_COEFF= 0.001`
`177`	`177`	`%`
`178`	`178`	`% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)`
`179`	`179`	`TIME_DISCRE_FLOW= EULER_IMPLICIT`
`180`		`-%`
`181`		`-% Relaxation coefficient`
`182`		`-RELAXATION_FACTOR_FLOW= 0.95`
`183`	`180`
`184`	`181`	`% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%`
`185`	`182`	`%`
`@@ -191,9 +188,6 @@ TIME_DISCRE_TURB= EULER_IMPLICIT`
`191`	`188`	`%`
`192`	`189`	`% Reduction factor of the CFL coefficient in the turbulence problem`
`193`	`190`	`CFL_REDUCTION_TURB= 1.0`
`194`		`-%`
`195`		`-% Relaxation coefficient`
`196`		`-RELAXATION_FACTOR_TURB= 0.95`
`197`	`191`
`198`	`192`	`% ---------------- ADJOINT-FLOW NUMERICAL METHOD DEFINITION -------------------%`
`199`	`193`	`%`