Removing unnecessary config options in CHT tutorial (to improve readability).

Author: oleburghardt

Inc_Heated_Cylinders/flow_cylinder.cfg

@@ -1,7 +1,7 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %                                                                              %
 % SU2 configuration file                                                       %
-% Case description: Steady incompressible laminar flow around a heated cylinder%
+% Case description: Steady incompressible laminar flow around heated cylinders %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -63,7 +63,7 @@ INC_DENSITY_MODEL= VARIABLE
 INC_ENERGY_EQUATION = YES
 %
 % Initial density for incompressible flows (1.2886 kg/m^3 by default)
-INC_DENSITY_INIT= 0.00042
+INC_DENSITY_INIT= 0.000210322
 %
 % Initial velocity for incompressible flows (1.0,0,0 m/s by default)
 INC_VELOCITY_INIT= ( 3.40297, 0.0, 0.0 )
@@ -123,19 +123,6 @@ PRANDTL_LAM= 0.72
 % Turbulent Prandtl number (0.9 (air), only for CONSTANT_PRANDTL)
 PRANDTL_TURB= 0.90
 
-% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
-%
-% Reference origin for moment computation
-REF_ORIGIN_MOMENT_X = 0.25
-REF_ORIGIN_MOMENT_Y = 0.00
-REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
-REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
-REF_AREA= 1.0
-
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
 % Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
@@ -154,58 +141,6 @@ CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
 % Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
-% ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
-VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the adjoint sharp edges limiter (3.0 by default).
-ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Freeze the value of the limiter after a number of iterations
-LIMITER_ITER= 999999
-%
-% 1st order artificial dissipation coefficients for
-%     the Lax–Friedrichs method ( 0.15 by default )
-LAX_SENSOR_COEFF= 0.15
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
-JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% 1st order artificial dissipation coefficients for
-%     the adjoint Lax–Friedrichs method ( 0.15 by default )
-ADJ_LAX_SENSOR_COEFF= 0.15
-%
-% 2nd, and 4th order artificial dissipation coefficients for
-%     the adjoint JST method ( 0.5, 0.02 by default )
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 % Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
@@ -225,10 +160,6 @@ LINEAR_SOLVER_ERROR= 1E-15
 % Max number of iterations of the linear solver for the implicit formulation
 LINEAR_SOLVER_ITER= 5
 
-% -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
-
-TIME_DISCRE_HEAT= EULER_IMPLICIT
-
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 % Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,

Inc_Heated_Cylinders/solid_cylinder1.cfg

@@ -1,7 +1,7 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %                                                                              %
 % SU2 configuration file                                                       %
-% Case description: Steady incompressible laminar flow around a heated cylinder%
+% Case description: Steady incompressible laminar flow around heated cylinders %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -56,36 +56,13 @@ SOLID_TEMPERATURE_INIT= 350.0
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
 %
 % Solid density (kg/m^3)
-SOLID_DENSITY= 0.00042
+SOLID_DENSITY= 0.000210322
 %
 % Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP_SOLID = 1004.703
 %
 % Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_SOLID= 0.1028
-%
-% aluminum
-%SOLID_DENSITY= 2700
-%SPECIFIC_HEAT_CP_SOLID = 921.096
-%THERMAL_CONDUCTIVITY_SOLID= 205.0
-%
-% glass
-%SOLID_DENSITY= 2700
-%SPECIFIC_HEAT_CP_SOLID = 840.0
-%THERMAL_CONDUCTIVITY_SOLID= 0.8
-
-% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
-%
-% Reference origin for moment computation
-REF_ORIGIN_MOMENT_X = 0.25
-REF_ORIGIN_MOMENT_Y = 0.00
-REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
-REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
-REF_AREA= 1.0
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
@@ -105,58 +82,6 @@ CFL_ADAPT_PARAM= ( 1.5, 0.5, 10.0, 10000.0 )
 % Runge-Kutta alpha coefficients
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
-% ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
-VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the adjoint sharp edges limiter (3.0 by default).
-ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Freeze the value of the limiter after a number of iterations
-LIMITER_ITER= 999999
-%
-% 1st order artificial dissipation coefficients for
-%     the Lax–Friedrichs method ( 0.15 by default )
-LAX_SENSOR_COEFF= 0.15
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
-JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% 1st order artificial dissipation coefficients for
-%     the adjoint Lax–Friedrichs method ( 0.15 by default )
-ADJ_LAX_SENSOR_COEFF= 0.15
-%
-% 2nd, and 4th order artificial dissipation coefficients for
-%     the adjoint JST method ( 0.5, 0.02 by default )
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 % Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
@@ -177,25 +102,8 @@ LINEAR_SOLVER_ERROR= 1E-15
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
-
-TIME_DISCRE_HEAT= EULER_IMPLICIT
-
-% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
-CONV_NUM_METHOD_FLOW= FDS
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
-MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
-SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
-TIME_DISCRE_FLOW= EULER_IMPLICIT
+TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %

Inc_Heated_Cylinders/solid_cylinder2.cfg

@@ -1,7 +1,7 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %                                                                              %
 % SU2 configuration file                                                       %
-% Case description: Steady incompressible laminar flow around a heated cylinder%
+% Case description: Steady incompressible laminar flow around heated cylinders %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -56,36 +56,13 @@ SOLID_TEMPERATURE_INIT= 350.0
 % Nettis case: hollow cylinder (air w/ 4x the conductivity)
 %
 % Solid density (kg/m^3)
-SOLID_DENSITY= 0.00042
+SOLID_DENSITY= 0.000210322
 %
 % Solid specific heat (J/kg*K)
 SPECIFIC_HEAT_CP_SOLID = 1004.703
 %
 % Solid thermal conductivity (W/m*K)
 THERMAL_CONDUCTIVITY_SOLID= 0.1028
-%
-% aluminum
-%SOLID_DENSITY= 2700
-%SPECIFIC_HEAT_CP_SOLID = 921.096
-%THERMAL_CONDUCTIVITY_SOLID= 205.0
-%
-% glass
-%SOLID_DENSITY= 2700
-%SPECIFIC_HEAT_CP_SOLID = 840.0
-%THERMAL_CONDUCTIVITY_SOLID= 0.8
-
-% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
-%
-% Reference origin for moment computation
-REF_ORIGIN_MOMENT_X = 0.25
-REF_ORIGIN_MOMENT_Y = 0.00
-REF_ORIGIN_MOMENT_Z = 0.00
-%
-% Reference length for pitching, rolling, and yawing non-dimensional moment
-REF_LENGTH= 1.0
-%
-% Reference area for force coefficients (0 implies automatic calculation)
-REF_AREA= 1.0
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
@@ -114,58 +91,6 @@ RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
 %                                             INVERSE_DESIGN_HEATFLUX, SURFACE_TOTAL_PRESSURE,
 %                                             SURFACE_MASSFLOW, SURFACE_STATIC_PRESSURE, SURFACE_MACH)
 
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-%
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 0
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 1, 1, 1 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.8
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.8
-
-% ----------- SLOPE LIMITER AND DISSIPATION SENSOR DEFINITION -----------------%
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
-VENKAT_LIMITER_COEFF= 0.05
-%
-% Coefficient for the adjoint sharp edges limiter (3.0 by default).
-ADJ_SHARP_LIMITER_COEFF= 3.0
-%
-% Freeze the value of the limiter after a number of iterations
-LIMITER_ITER= 999999
-%
-% 1st order artificial dissipation coefficients for
-%     the Lax–Friedrichs method ( 0.15 by default )
-LAX_SENSOR_COEFF= 0.15
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
-JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% 1st order artificial dissipation coefficients for
-%     the adjoint Lax–Friedrichs method ( 0.15 by default )
-ADJ_LAX_SENSOR_COEFF= 0.15
-%
-% 2nd, and 4th order artificial dissipation coefficients for
-%     the adjoint JST method ( 0.5, 0.02 by default )
-ADJ_JST_SENSOR_COEFF= ( 0.5, 0.02 )
-
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 % Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER_JACOBI,
@@ -186,25 +111,9 @@ LINEAR_SOLVER_ERROR= 1E-15
 LINEAR_SOLVER_ITER= 5
 
 % -------------------- HEAT NUMERICAL METHOD DEFINITION -----------------------%
-
-TIME_DISCRE_HEAT= EULER_IMPLICIT
-
-% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
-%
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
-CONV_NUM_METHOD_FLOW= FDS
 %
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
-MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
-SLOPE_LIMITER_FLOW= NONE
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
-TIME_DISCRE_FLOW= EULER_IMPLICIT
+% Time discretization (EULER_IMPLICIT, EULER_EXPLICIT)
+TIME_DISCRE_HEAT= EULER_IMPLICIT
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 %