Adapting tutorial cases

talbring · talbring · commit 99449cda43fb · 2019-08-09T17:55:35.000+02:00
diff --git a/Inc_Inviscid_Hydrofoil/inv_naca0012.cfg b/Inc_Inviscid_Hydrofoil/inv_naca0012.cfg
@@ -13,10 +13,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)                           
-PHYSICAL_PROBLEM= EULER
-%
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE)
-REGIME_TYPE= INCOMPRESSIBLE
+SOLVER= INC_EULER
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
diff --git a/Inc_Laminar_Cavity/lam_buoyancy_cavity.cfg b/Inc_Laminar_Cavity/lam_buoyancy_cavity.cfg
@@ -13,10 +13,8 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= INC_NAVIER_STOKES
 %
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE, FREESURFACE)
-REGIME_TYPE= INCOMPRESSIBLE
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
diff --git a/Inc_Laminar_Flat_Plate/lam_flatplate.cfg b/Inc_Laminar_Flat_Plate/lam_flatplate.cfg
@@ -13,14 +13,11 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= INC_NAVIER_STOKES
 %
 % Specify turbulence model (NONE, SA)
 KIND_TURB_MODEL= NONE
 %
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE)
-REGIME_TYPE= INCOMPRESSIBLE
-%
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
 %
diff --git a/Inc_Laminar_Step/lam_backwardstep.cfg b/Inc_Laminar_Step/lam_backwardstep.cfg
@@ -13,14 +13,11 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= INC_NAVIER_STOKES
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
 %
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE, FREESURFACE)
-REGIME_TYPE= INCOMPRESSIBLE
-%
 % Restart solution (NO, YES)
 RESTART_SOL= NO
 
diff --git a/Inc_Turbulent_Flat_Plate/turb_flatplate.cfg b/Inc_Turbulent_Flat_Plate/turb_flatplate.cfg
@@ -13,14 +13,11 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= INC_NAVIER_STOKES
 %
 % If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= SA
 %
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE)
-REGIME_TYPE= INCOMPRESSIBLE
-%
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
 %
diff --git a/Inc_Turbulent_NACA0012/turb_naca0012.cfg b/Inc_Turbulent_NACA0012/turb_naca0012.cfg
@@ -14,17 +14,14 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= INC_NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
 %
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE, FREESURFACE)
-REGIME_TYPE= INCOMPRESSIBLE
-%
 % Restart solution (NO, YES)
 RESTART_SOL= NO
 
diff --git a/Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg b/Inviscid_2D_Unconstrained_NACA0012/inv_NACA0012_basic.cfg
@@ -14,7 +14,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION) 
-PHYSICAL_PROBLEM= EULER
+SOLVER= EULER
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
diff --git a/Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg b/Inviscid_3D_Constrained_ONERAM6/inv_ONERAM6_adv.cfg
@@ -14,7 +14,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= EULER
+SOLVER= EULER
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DISCRETE_ADJOINT
diff --git a/Inviscid_Bump/inv_channel.cfg b/Inviscid_Bump/inv_channel.cfg
@@ -13,7 +13,7 @@
 %
 % Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)
 %                               
-PHYSICAL_PROBLEM= EULER
+SOLVER= EULER
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
diff --git a/Inviscid_ONERAM6/inv_ONERAM6.cfg b/Inviscid_ONERAM6/inv_ONERAM6.cfg
@@ -12,7 +12,7 @@
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
 % Physical governing equations (EULER, NAVIER_STOKES)
-PHYSICAL_PROBLEM= EULER
+SOLVER= EULER
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
diff --git a/Inviscid_Wedge/inv_wedge_HLLC.cfg b/Inviscid_Wedge/inv_wedge_HLLC.cfg
@@ -14,7 +14,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= EULER
+SOLVER= EULER
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
diff --git a/Laminar_Cylinder/lam_cylinder.cfg b/Laminar_Cylinder/lam_cylinder.cfg
@@ -14,7 +14,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
diff --git a/Laminar_Flat_Plate/lam_flatplate.cfg b/Laminar_Flat_Plate/lam_flatplate.cfg
@@ -14,7 +14,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
diff --git a/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg b/Multi_Objective_Shape_Design/inv_wedge_ROE_multiobj_combo.cfg
@@ -20,7 +20,7 @@
 %                               TNE2_EULER, TNE2_NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= EULER
+SOLVER= EULER
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= CONTINUOUS_ADJOINT
diff --git a/NICFD_nozzle/NICFD_nozzle.cfg b/NICFD_nozzle/NICFD_nozzle.cfg
@@ -16,17 +16,14 @@
 %                               FEM_EULER, FEM_NAVIER_STOKES, FEM_RANS, FEM_LES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulence model (NONE, SA, SA_NEG, SST, SA_E, SA_COMP, SA_E_COMP)
 KIND_TURB_MODEL= SST
 %
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
 MATH_PROBLEM= DIRECT
 %
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE)
-REGIME_TYPE= COMPRESSIBLE
-%
 % Restart solution (NO, YES)
 RESTART_SOL= NO
 %
diff --git a/Transitional_Flat_Plate/transitional_BC_model_ConfigFile.cfg b/Transitional_Flat_Plate/transitional_BC_model_ConfigFile.cfg
@@ -15,7 +15,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= INC_NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
@@ -27,9 +27,6 @@ FREESTREAM_TURBULENCEINTENSITY = 0.18
 % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
 MATH_PROBLEM= DIRECT
 %
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE, FREESURFACE)
-REGIME_TYPE= INCOMPRESSIBLE
-%
 % Restart solution (NO, YES)
 RESTART_SOL= NO
 
diff --git a/Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg b/Turbulent_2D_Constrained_RAE2822/turb_SA_RAE2822.cfg
@@ -14,7 +14,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)                              
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
diff --git a/Turbulent_Flat_Plate/turb_SA_flatplate.cfg b/Turbulent_Flat_Plate/turb_SA_flatplate.cfg
@@ -14,7 +14,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % If Navier-Stokes, kind of turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
diff --git a/Turbulent_ONERAM6/turb_ONERAM6.cfg b/Turbulent_ONERAM6/turb_ONERAM6.cfg
@@ -14,7 +14,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)          
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
diff --git a/UQ_NACA0012/turb_NACA0012_uq.cfg b/UQ_NACA0012/turb_NACA0012_uq.cfg
@@ -15,7 +15,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)                             
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
diff --git a/UQ_NACA0012/turb_NACA0012_uq_1c.cfg b/UQ_NACA0012/turb_NACA0012_uq_1c.cfg
@@ -15,7 +15,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)                             
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
diff --git a/UQ_NACA0012/turb_NACA0012_uq_2c.cfg b/UQ_NACA0012/turb_NACA0012_uq_2c.cfg
@@ -15,7 +15,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)                             
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
diff --git a/UQ_NACA0012/turb_NACA0012_uq_3c.cfg b/UQ_NACA0012/turb_NACA0012_uq_3c.cfg
@@ -15,7 +15,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)                             
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
diff --git a/UQ_NACA0012/turb_NACA0012_uq_p1c1.cfg b/UQ_NACA0012/turb_NACA0012_uq_p1c1.cfg
@@ -15,7 +15,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)                             
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
diff --git a/UQ_NACA0012/turb_NACA0012_uq_p1c2.cfg b/UQ_NACA0012/turb_NACA0012_uq_p1c2.cfg
@@ -15,7 +15,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)                             
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SST
diff --git a/_tutorials/compressible_flow/Laminar_Flat_Plate.md b/_tutorials/compressible_flow/Laminar_Flat_Plate.md
@@ -71,13 +71,13 @@ Several of the key configuration file options for this simulation are highlighte
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= NONE
 ```
 
-To compute viscous flows, the Navier-Stokes governing equations are selected. In conjunction with selecting Navier-Stokes as the problem type, the type of turbulence model must also be specified. Laminar flows can be computed by entering `KIND_TURB_MODEL= NONE`. For turbulent flows, SU2 currently contains implementations of the Spalart-Allmaras model (`SA`, `SA_NEG`) and the Shear Stress Transport (`SST`) model of Menter. If this were an inviscid flow problem, the user would enter `PHYSICAL_PROBLEM = EULER` for the problem type. SU2 supports other governing equations, as well, and the user is invited to review the configuration page for a description of the possible options.
+To compute viscous flows, the Navier-Stokes governing equations are selected. In conjunction with selecting Navier-Stokes as the problem type, the type of turbulence model must also be specified. Laminar flows can be computed by entering `KIND_TURB_MODEL= NONE`. For turbulent flows, SU2 currently contains implementations of the Spalart-Allmaras model (`SA`, `SA_NEG`) and the Shear Stress Transport (`SST`) model of Menter. If this were an inviscid flow problem, the user would enter `SOLVER = EULER` for the problem type. SU2 supports other governing equations, as well, and the user is invited to review the configuration page for a description of the possible options.
 
 Defining a no-slip boundary condition for viscous walls can be accomplished in one of two ways:
 
diff --git a/_tutorials/compressible_flow/NICFD_nozzle.md b/_tutorials/compressible_flow/NICFD_nozzle.md
@@ -67,7 +67,7 @@ The governing equations are Navier-Stokes, but by entering `KIND_TURB_MODEL= SST
 %                               FEM_EULER, FEM_NAVIER_STOKES, FEM_RANS, FEM_LES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulence model (NONE, SA, SA_NEG, SST, SA_E, SA_COMP, SA_E_COMP)
 KIND_TURB_MODEL= SST
diff --git a/_tutorials/compressible_flow/Transitional_Flat_Plate.md b/_tutorials/compressible_flow/Transitional_Flat_Plate.md
@@ -51,7 +51,7 @@ Several of the key configuration file options for this simulation are highlighte
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, 
 %                               LINEAR_ELASTICITY, POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulent model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
@@ -61,9 +61,6 @@ KIND_TRANS_MODEL= BC
 %
 % Specify Turbulence Intensity (%)
 FREESTREAM_TURBULENCEINTENSITY = 0.18
-%
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE, FREESURFACE)
-REGIME_TYPE= INCOMPRESSIBLE
 ```
 
 The governing equations are RANS with the Spalart-Allmaras (`SA`) turbulence model. By entering `KIND_TRANS_MODEL= BC`, the Bas-Cakmakcioglu Algebraic Transition Model is activated. This model requires freestream turbulence intensity that is to be used in the transition correlation, thus the `FREESTREAM_TURBULENCEINTENSITY` option is also used. The BC model achieves its purpose by modifying the production term of the 1-equation SA turbulence model. The production term of the SA model is damped until a considerable amount of turbulent viscosity is generated, and after that point, the damping effect on the transition model is disabled. Thus, a transition from laminar to turbulent flow is obtained.
diff --git a/_tutorials/compressible_flow/Turbulent_Flat_Plate.md b/_tutorials/compressible_flow/Turbulent_Flat_Plate.md
@@ -54,7 +54,7 @@ Several of the key configuration file options for this simulation are highlighte
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
diff --git a/_tutorials/incompressible_flow/Inc_Inviscid_Hydrofoil.md b/_tutorials/incompressible_flow/Inc_Inviscid_Hydrofoil.md
@@ -42,11 +42,11 @@ The mesh is composed of 6814 triangles with 3559 vertices in total, 128 edges al
 
 ### Configuration File Options
 
-In order to use the incompressible solver, the flow regime should first be switched from COMPRESSIBLE (default) to INCOMPRESSIBLE with the following option:
+In order to use the incompressible solver, choose the appropriate setting with the `SOLVER` option:
 
 ```
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE)
-REGIME_TYPE= INCOMPRESSIBLE
+% Solver type
+REGIME_TYPE= INC_EULER
 ```
  
 Once the incompressible mode is activated, the flow throughout the domain is initialized using a different set of options as compared to the compressible mode. The present problem is inviscid (no energy equation), so the only required initialization data is the density (constant) and flow velocity. These initialization values are set with the following options:
diff --git a/_tutorials/incompressible_flow/Inc_Turbulent_Flat_Plate.md b/_tutorials/incompressible_flow/Inc_Turbulent_Flat_Plate.md
@@ -51,13 +51,10 @@ Several of the key configuration file options for this simulation are highlighte
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
 %
 % Physical governing equations (EULER, NAVIER_STOKES, ...
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= INC_NAVIER_STOKES
 %
 % If Navier-Stokes, kind of turbulent model (NONE, SA)
 KIND_TURB_MODEL= SA
-%
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE)
-REGIME_TYPE= INCOMPRESSIBLE
 ```
 
 We activate the turbulence model using the same options as for the compressible solver. Here, we employ the SA model, but all turbulence models available for the compressible solver can also be used with the incompressible version. The selection of numerical methods for the turbulence equations and other parameters unique to the turbulence models are set using the same options covered by previous compressible tutorials.
diff --git a/documents/turb_hl_crm.cfg b/documents/turb_hl_crm.cfg
@@ -13,7 +13,7 @@
 % Physical governing equations (EULER, NAVIER_STOKES,
 %                               WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
 %                               POISSON_EQUATION)
-PHYSICAL_PROBLEM= NAVIER_STOKES
+SOLVER= NAVIER_STOKES
 %
 % Specify turbulence model (NONE, SA, SA_NEG, SST)
 KIND_TURB_MODEL= SA
@@ -24,9 +24,6 @@ MATH_PROBLEM= DIRECT
 % Restart solution (NO, YES)
 RESTART_SOL= NO
 %
-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE)
-REGIME_TYPE= COMPRESSIBLE
-%
 % System of measurements (SI, US)
 % International system of units (SI): ( meters, kilograms, Kelvins,
 %                                       Newtons = kg m/s^2, Pascals = N/m^2, 

Original file line number	Diff line number	Diff line change
`@@ -13,10 +13,8 @@`
`13`	`13`	`% Physical governing equations (EULER, NAVIER_STOKES,`
`14`	`14`	`% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,`
`15`	`15`	`% POISSON_EQUATION)`
`16`		`-PHYSICAL_PROBLEM= NAVIER_STOKES`
	`16`	`+SOLVER= INC_NAVIER_STOKES`
`17`	`17`	`%`
`18`		`-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE, FREESURFACE)`
`19`		`-REGIME_TYPE= INCOMPRESSIBLE`
`20`	`18`	`%`
`21`	`19`	`% Specify turbulent model (NONE, SA, SA_NEG, SST)`
`22`	`20`	`KIND_TURB_MODEL= NONE`
Original file line number	Diff line number	Diff line change
`@@ -13,14 +13,11 @@`
`13`	`13`	`% Physical governing equations (EULER, NAVIER_STOKES,`
`14`	`14`	`% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,`
`15`	`15`	`% POISSON_EQUATION)`
`16`		`-PHYSICAL_PROBLEM= NAVIER_STOKES`
	`16`	`+SOLVER= INC_NAVIER_STOKES`
`17`	`17`	`%`
`18`	`18`	`% Specify turbulence model (NONE, SA)`
`19`	`19`	`KIND_TURB_MODEL= NONE`
`20`	`20`	`%`
`21`		`-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE)`
`22`		`-REGIME_TYPE= INCOMPRESSIBLE`
`23`		`-%`
`24`	`21`	`% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)`
`25`	`22`	`MATH_PROBLEM= DIRECT`
`26`	`23`	`%`
Original file line number	Diff line number	Diff line change
`@@ -14,17 +14,14 @@`
`14`	`14`	`% Physical governing equations (EULER, NAVIER_STOKES,`
`15`	`15`	`% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,`
`16`	`16`	`% POISSON_EQUATION)`
`17`		`-PHYSICAL_PROBLEM= NAVIER_STOKES`
	`17`	`+SOLVER= INC_NAVIER_STOKES`
`18`	`18`	`%`
`19`	`19`	`% Specify turbulent model (NONE, SA, SA_NEG, SST)`
`20`	`20`	`KIND_TURB_MODEL= SA`
`21`	`21`	`%`
`22`	`22`	`% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)`
`23`	`23`	`MATH_PROBLEM= DIRECT`
`24`	`24`	`%`
`25`		`-% Regime type (COMPRESSIBLE, INCOMPRESSIBLE, FREESURFACE)`
`26`		`-REGIME_TYPE= INCOMPRESSIBLE`
`27`		`-%`
`28`	`25`	`% Restart solution (NO, YES)`
`29`	`26`	`RESTART_SOL= NO`
`30`	`27`
Original file line number	Diff line number	Diff line change
`@@ -14,7 +14,7 @@`
`14`	`14`	`% Physical governing equations (EULER, NAVIER_STOKES,`
`15`	`15`	`% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,`
`16`	`16`	`% POISSON_EQUATION)`
`17`		`-PHYSICAL_PROBLEM= EULER`
	`17`	`+SOLVER= EULER`
`18`	`18`	`%`
`19`	`19`	`% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)`
`20`	`20`	`MATH_PROBLEM= DIRECT`
Original file line number	Diff line number	Diff line change
`@@ -13,7 +13,7 @@`
`13`	`13`	`%`
`14`	`14`	`% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)`
`15`	`15`	`%`
`16`		`-PHYSICAL_PROBLEM= EULER`
	`16`	`+SOLVER= EULER`
`17`	`17`	`%`
`18`	`18`	`% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)`
`19`	`19`	`MATH_PROBLEM= DIRECT`
Original file line number	Diff line number	Diff line change
`@@ -12,7 +12,7 @@`
`12`	`12`	`% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%`
`13`	`13`	`%`
`14`	`14`	`% Physical governing equations (EULER, NAVIER_STOKES)`
`15`		`-PHYSICAL_PROBLEM= EULER`
	`15`	`+SOLVER= EULER`
`16`	`16`	`%`
`17`	`17`	`% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)`
`18`	`18`	`MATH_PROBLEM= DIRECT`