minor fixes

jayantmukho · jayantmukho · commit ad132e89ea33 · 2019-09-24T00:03:52.000-07:00
diff --git a/Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg b/Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg
@@ -36,7 +36,7 @@ FREESTREAM_PRESSURE= 101325.0
 % Free-stream temperature (288.15 K by default)
 FREESTREAM_TEMPERATURE= 288.15
 
-% -------------------------- CL & CM DRIVER DEFINITION ------------------------%
+% -------------------------- CL DRIVER DEFINITION -----------------------------%
 %
 % Activate fixed lift mode (specify a CL instead of AoA, NO/YES)
 FIXED_CL_MODE= YES 
diff --git a/Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg b/Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg
@@ -42,7 +42,7 @@ REYNOLDS_NUMBER= 6.5E6
 % Reynolds length (1 m by default)
 REYNOLDS_LENGTH= 1.0
 
-% -------------------------- CL & CM DRIVER DEFINITION ------------------------%
+% -------------------------- CL DRIVER DEFINITION -----------------------------%
 %
 % Activate fixed lift mode (specify a CL instead of AoA, NO/YES)
 FIXED_CL_MODE= YES
diff --git a/_tutorials/design_features/Inviscid_2D_Unconstrained_NACA0012.md b/_tutorials/design_features/Inviscid_2D_Unconstrained_NACA0012.md
@@ -133,7 +133,7 @@ The `DEFINITION_DV` is the list of design variables. For the airfoil problem, we
 
 It is quite common to introduce angle of attack as a design variable (with a given Cl). In that case, you should add to the config file the following extra information:
 ```
-% -------------------------- CL & CM DRIVER DEFINITION ------------------------%
+% -------------------------- CL DRIVER DEFINITION -----------------------------%
 %
 % Activate fixed lift mode (specify a CL instead of AoA, NO/YES)
 FIXED_CL_MODE= YES
diff --git a/_tutorials/design_features/Inviscid_3D_Constrained_ONERAM6.md b/_tutorials/design_features/Inviscid_3D_Constrained_ONERAM6.md

Original file line number	Diff line number	Diff line change
`@@ -36,7 +36,7 @@ FREESTREAM_PRESSURE= 101325.0`
`36`	`36`	`% Free-stream temperature (288.15 K by default)`
`37`	`37`	`FREESTREAM_TEMPERATURE= 288.15`
`38`	`38`
`39`		`-% -------------------------- CL & CM DRIVER DEFINITION ------------------------%`
	`39`	`+% -------------------------- CL DRIVER DEFINITION -----------------------------%`
`40`	`40`	`%`
`41`	`41`	`% Activate fixed lift mode (specify a CL instead of AoA, NO/YES)`
`42`	`42`	`FIXED_CL_MODE= YES`
Original file line number	Diff line number	Diff line change
`@@ -42,7 +42,7 @@ REYNOLDS_NUMBER= 6.5E6`
`42`	`42`	`% Reynolds length (1 m by default)`
`43`	`43`	`REYNOLDS_LENGTH= 1.0`
`44`	`44`
`45`		`-% -------------------------- CL & CM DRIVER DEFINITION ------------------------%`
	`45`	`+% -------------------------- CL DRIVER DEFINITION -----------------------------%`
`46`	`46`	`%`
`47`	`47`	`% Activate fixed lift mode (specify a CL instead of AoA, NO/YES)`
`48`	`48`	`FIXED_CL_MODE= YES`
Original file line number	Diff line number	Diff line change
@@ -133,7 +133,7 @@ The `DEFINITION_DV` is the list of design variables. For the airfoil problem, we
`133`	`133`
`134`	`134`	`It is quite common to introduce angle of attack as a design variable (with a given Cl). In that case, you should add to the config file the following extra information:`
`135`	`135`	```
`136`		`-% -------------------------- CL & CM DRIVER DEFINITION ------------------------%`
	`136`	`+% -------------------------- CL DRIVER DEFINITION -----------------------------%`
`137`	`137`	`%`
`138`	`138`	`% Activate fixed lift mode (specify a CL instead of AoA, NO/YES)`
`139`	`139`	`FIXED_CL_MODE= YES`