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README.md

@@ -123,4 +123,5 @@ The nested structure ensures that increasing dataset size refines sampling densi
 
 ## Note:
 
-Part of the dataset, due to HF dataset size limit, is in a seperate repo double-delta-aero2
+The license is different from manuscript (From LGPL2.1 to CC-BY-2.0). https://arc.aiaa.org/doi/abs/10.2514/6.2026-0686 OR https://arxiv.org/abs/2512.20941
+Please refer to the publication for details.

example/11.0degAOA/config.cfg

@@ -0,0 +1,114 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= RANS
+KIND_TURB_MODEL= SA
+SA_OPTIONS= ROTATION
+RESTART_SOL= NO
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.3
+AOA= 11.0
+FREESTREAM_TEMPERATURE= 285.0
+REYNOLDS_NUMBER= 8.04E7
+REYNOLDS_LENGTH= 16
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 13.063688846316008
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 16
+REF_AREA= 659.6039695925111
+
+% --------------------FLUID MODEL----------------------------------------------%
+%
+FLUID_MODEL= STANDARD_AIR
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.058
+
+% -----------------------VISCOSITY MODEL--------------------------------------%
+%
+VISCOSITY_MODEL= SUTHERLAND
+MU_CONSTANT=1.716e-05
+
+% --------------------------THERMAL MODEL-------------------------------------%
+%
+CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
+PRANDTL_LAM= 0.72
+PRANDTL_TURB= 0.90
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( wall, 0.0 )
+%MARKER_EULER= ( wall )
+MARKER_FAR= ( farfield )
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+FREESTREAM_TURBULENCEINTENSITY= 0.03
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 10.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.2, 1.5, 0.00001, 2000 )
+ITER= 29999
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_ERROR= 1E-7
+LINEAR_SOLVER_ITER= 50
+LINEAR_SOLVER_PREC= ILU
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+MGCYCLE= W_CYCLE
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+MG_DAMP_RESTRICTION= 0.95
+MG_DAMP_PROLONGATION= 0.95
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= JST
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.08
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+MUSCL_TURB= NO
+SLOPE_LIMITER_TURB= VENKATAKRISHNAN
+TIME_DISCRE_TURB= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -6
+CONV_STARTITER= 800
+CONV_FIELD= DRAG
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-5
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= /scratch/users/yrshen/scitec26/geom256samples/020701-1VN.su2
+MESH_FORMAT= SU2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow.dat
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+VOLUME_FILENAME= flow
+SURFACE_FILENAME= surface_flow
+OUTPUT_WRT_FREQ= 200
+WRT_FORCES_BREAKDOWN= YES
+BREAKDOWN_FILENAME= forces_breakdown.dat
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+HISTORY_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+% Change to Tecplot if needed
+VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRIMITIVE, DISSIPATION, MESH_QUALITY)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW, SURFACE_PARAVIEW_ASCII)

example/11.0degAOA/forces_breakdown.dat

@@ -0,0 +1,129 @@
+
+-------------------------------------------------------------------------
+|    ___ _   _ ___                                                      |
+|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
+|   \__ \ |_| |/ /                                                      |
+|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
+|                                                                       |
+-------------------------------------------------------------------------
+| SU2 Project Website: https://su2code.github.io                        |
+|                                                                       |
+| The SU2 Project is maintained by the SU2 Foundation                   |
+| (http://su2foundation.org)                                            |
+-------------------------------------------------------------------------
+| Copyright 2012-2023, SU2 Contributors                                 |
+|                                                                       |
+| SU2 is free software; you can redistribute it and/or                  |
+| modify it under the terms of the GNU Lesser General Public            |
+| License as published by the Free Software Foundation; either          |
+| version 2.1 of the License, or (at your option) any later version.    |
+|                                                                       |
+| SU2 is distributed in the hope that it will be useful,                |
+| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
+| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
+| Lesser General Public License for more details.                       |
+|                                                                       |
+| You should have received a copy of the GNU Lesser General Public      |
+| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
+-------------------------------------------------------------------------
+
+
+Problem definition:
+
+Compressible RANS equations.
+Turbulence model: Spalart Allmaras
+Mach number: 0.3.
+Angle of attack (AoA): 11 deg, and angle of sideslip (AoS): 0 deg.
+Reynolds number: 8.04e+07.
+Dimensional simulation.
+The reference area is 659.604 m^2.
+The reference length is 16 m.
+
+
+Problem definition:
+
+Viscous flow: Computing pressure using the ideal gas law
+based on the free-stream temperature and a density computed
+from the Reynolds number.
+Force coefficients computed using free-stream values.
+-- Input conditions:
+Fluid Model: STANDARD_AIR 
+Specific gas constant: 287.058 N.m/kg.K.
+Specific gas constant (non-dim): 287.058
+Specific Heat Ratio: 1.4000 
+Viscosity Model: SUTHERLAND 
+Ref. Laminar Viscosity: 1.716e-05 N.s/m^2.
+Ref. Temperature: 273.15 K.
+Sutherland Constant: 110.4 K.
+Laminar Viscosity (non-dim): 1.716e-05
+Ref. Temperature (non-dim): 273.15
+Sutherland constant (non-dim): 110.4
+Conductivity Model: CONSTANT_PRANDTL 
+Prandtl: 0.72
+Turbulent Conductivity Model: CONSTANT_PRANDTL 
+Turbulent Prandtl: 0.9
+Free-stream static pressure: 71833.4 Pa.
+Free-stream total pressure: 76461.6 Pa.
+Free-stream temperature: 285 K.
+Free-stream total temperature: 290.13 K.
+Free-stream density: 0.878035 kg/m^3.
+Free-stream velocity: (99.6642, 0, 19.3728) m/s. Magnitude: 101.53 m/s.
+Free-stream total energy per unit mass: 209683 m^2/s^2.
+Free-stream viscosity: 1.77406e-05 N.s/m^2.
+Free-stream turb. kinetic energy per unit mass: 13.9161 m^2/s^2.
+Free-stream specific dissipation: 68875.1 1/s.
+-- Reference values:
+Reference specific gas constant: 1 N.m/kg.K.
+Reference pressure: 1 Pa.
+Reference temperature: 1 K.
+Reference density: 1 kg/m^3.
+Reference velocity: 1 m/s.
+Reference energy per unit mass: 1 m^2/s^2.
+Reference viscosity: 1 N.s/m^2.
+Reference conductivity: 1 W/m^2.K.
+-- Resulting non-dimensional state:
+Mach number (non-dim): 0.3
+Reynolds number (non-dim): 8.04e+07. Re length: 16 m.
+Specific gas constant (non-dim): 287.058
+Free-stream temperature (non-dim): 285
+Free-stream pressure (non-dim): 71833.4
+Free-stream density (non-dim): 0.878035
+Free-stream velocity (non-dim): (99.6642, 0, 19.3728). Magnitude: 101.53
+Free-stream total energy per unit mass (non-dim): 209683
+Free-stream viscosity (non-dim): 1.77406e-05
+Free-stream turb. kinetic energy (non-dim): 13.9161
+Free-stream specific dissipation (non-dim): 68875.1
+
+
+Forces breakdown:
+
+Center of Pressure: X=-0.079610Z+33.300123 m.
+
+NOTE: Multiply forces by the non-dimensional factor: 2985038.585495, and the reference factor: 1.000000
+to obtain the dimensional force.
+
+Total CL:       0.474738 | Pressure (  100%):    0.475316 | Friction (    0%):   -0.000577 | Momentum (    0%):    0.000000
+Total CD:       0.053656 | Pressure (   91%):    0.049273 | Friction (    8%):    0.004382 | Momentum (    0%):    0.000000
+Total CSF:      0.000011 | Pressure (   93%):    0.000010 | Friction (    6%):    0.000001 | Momentum (    0%):    0.000000
+Total CL/CD:    8.847875 | Pressure (  109%):    9.646549 | Friction (   -1%):   -0.131754 | Momentum (    0%):    0.000000
+Total CMx:      0.000087 | Pressure (   99%):    0.000087 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy:     -0.602355 | Pressure (   99%):   -0.602195 | Friction (    0%):   -0.000160 | Momentum (    0%):    0.000000
+Total CMz:      0.000022 | Pressure (   91%):    0.000020 | Friction (    8%):    0.000002 | Momentum (    0%):    0.000000
+Total CFx:     -0.037914 | Pressure (  111%):   -0.042327 | Friction (  -11%):    0.004412 | Momentum (    0%):    0.000000
+Total CFy:      0.000011 | Pressure (   93%):    0.000010 | Friction (    6%):    0.000001 | Momentum (    0%):    0.000000
+Total CFz:      0.476254 | Pressure (   99%):    0.475984 | Friction (    0%):    0.000269 | Momentum (    0%):    0.000000
+
+
+Surface name: wall
+
+Total CL    (   99%):    0.474738 | Pressure (  100%):    0.475316 | Friction (    0%):   -0.000577 | Momentum (    0%):    0.000000
+Total CD    (   99%):    0.053656 | Pressure (   91%):    0.049273 | Friction (    8%):    0.004382 | Momentum (    0%):    0.000000
+Total CSF   (   99%):    0.000011 | Pressure (   93%):    0.000010 | Friction (    6%):    0.000001 | Momentum (    0%):    0.000000
+Total CL/CD (  100%):    8.847875 | Pressure (  109%):    9.646549 | Friction (   -1%):   -0.131754 | Momentum (    0%):    0.000000
+Total CMx   (   99%):    0.000087 | Pressure (   99%):    0.000087 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy   (  100%):   -0.602355 | Pressure (   99%):   -0.602195 | Friction (    0%):   -0.000160 | Momentum (    0%):    0.000000
+Total CMz   (   99%):    0.000022 | Pressure (   91%):    0.000020 | Friction (    8%):    0.000002 | Momentum (    0%):    0.000000
+Total CFx   (  100%):   -0.037914 | Pressure (  111%):   -0.042327 | Friction (  -11%):    0.004412 | Momentum (    0%):    0.000000
+Total CFy   (   99%):    0.000011 | Pressure (   93%):    0.000010 | Friction (    6%):    0.000001 | Momentum (    0%):    0.000000
+Total CFz   (   99%):    0.476254 | Pressure (   99%):    0.475984 | Friction (    0%):    0.000269 | Momentum (    0%):    0.000000
+

example/11.0degAOA/surface_and_volume_flow.zip

@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:bed3e01ae5836d5d01901cbc758405162ccd3dbe75594b3a255625382447d8c0
+size 230898459

example/12.0degAOA/config.cfg

@@ -0,0 +1,114 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= RANS
+KIND_TURB_MODEL= SA
+SA_OPTIONS= ROTATION
+RESTART_SOL= NO
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.3
+AOA= 12.0
+FREESTREAM_TEMPERATURE= 285.0
+REYNOLDS_NUMBER= 8.04E7
+REYNOLDS_LENGTH= 16
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 13.063688846316008
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 16
+REF_AREA= 659.6039695925111
+
+% --------------------FLUID MODEL----------------------------------------------%
+%
+FLUID_MODEL= STANDARD_AIR
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.058
+
+% -----------------------VISCOSITY MODEL--------------------------------------%
+%
+VISCOSITY_MODEL= SUTHERLAND
+MU_CONSTANT=1.716e-05
+
+% --------------------------THERMAL MODEL-------------------------------------%
+%
+CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
+PRANDTL_LAM= 0.72
+PRANDTL_TURB= 0.90
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( wall, 0.0 )
+%MARKER_EULER= ( wall )
+MARKER_FAR= ( farfield )
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+FREESTREAM_TURBULENCEINTENSITY= 0.03
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 10.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.2, 1.5, 0.00001, 2000 )
+ITER= 29999
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_ERROR= 1E-7
+LINEAR_SOLVER_ITER= 50
+LINEAR_SOLVER_PREC= ILU
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+MGCYCLE= W_CYCLE
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+MG_DAMP_RESTRICTION= 0.95
+MG_DAMP_PROLONGATION= 0.95
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= JST
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.08
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+MUSCL_TURB= NO
+SLOPE_LIMITER_TURB= VENKATAKRISHNAN
+TIME_DISCRE_TURB= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -6
+CONV_STARTITER= 800
+CONV_FIELD= DRAG
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-5
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= /scratch/users/yrshen/scitec26/geom256samples/020701-1VN.su2
+MESH_FORMAT= SU2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow.dat
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+VOLUME_FILENAME= flow
+SURFACE_FILENAME= surface_flow
+OUTPUT_WRT_FREQ= 200
+WRT_FORCES_BREAKDOWN= YES
+BREAKDOWN_FILENAME= forces_breakdown.dat
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+HISTORY_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+% Change to Tecplot if needed
+VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRIMITIVE, DISSIPATION, MESH_QUALITY)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW, SURFACE_PARAVIEW_ASCII)

example/12.0degAOA/forces_breakdown.dat

@@ -0,0 +1,129 @@
+
+-------------------------------------------------------------------------
+|    ___ _   _ ___                                                      |
+|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
+|   \__ \ |_| |/ /                                                      |
+|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
+|                                                                       |
+-------------------------------------------------------------------------
+| SU2 Project Website: https://su2code.github.io                        |
+|                                                                       |
+| The SU2 Project is maintained by the SU2 Foundation                   |
+| (http://su2foundation.org)                                            |
+-------------------------------------------------------------------------
+| Copyright 2012-2023, SU2 Contributors                                 |
+|                                                                       |
+| SU2 is free software; you can redistribute it and/or                  |
+| modify it under the terms of the GNU Lesser General Public            |
+| License as published by the Free Software Foundation; either          |
+| version 2.1 of the License, or (at your option) any later version.    |
+|                                                                       |
+| SU2 is distributed in the hope that it will be useful,                |
+| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
+| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
+| Lesser General Public License for more details.                       |
+|                                                                       |
+| You should have received a copy of the GNU Lesser General Public      |
+| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
+-------------------------------------------------------------------------
+
+
+Problem definition:
+
+Compressible RANS equations.
+Turbulence model: Spalart Allmaras
+Mach number: 0.3.
+Angle of attack (AoA): 12 deg, and angle of sideslip (AoS): 0 deg.
+Reynolds number: 8.04e+07.
+Dimensional simulation.
+The reference area is 659.604 m^2.
+The reference length is 16 m.
+
+
+Problem definition:
+
+Viscous flow: Computing pressure using the ideal gas law
+based on the free-stream temperature and a density computed
+from the Reynolds number.
+Force coefficients computed using free-stream values.
+-- Input conditions:
+Fluid Model: STANDARD_AIR 
+Specific gas constant: 287.058 N.m/kg.K.
+Specific gas constant (non-dim): 287.058
+Specific Heat Ratio: 1.4000 
+Viscosity Model: SUTHERLAND 
+Ref. Laminar Viscosity: 1.716e-05 N.s/m^2.
+Ref. Temperature: 273.15 K.
+Sutherland Constant: 110.4 K.
+Laminar Viscosity (non-dim): 1.716e-05
+Ref. Temperature (non-dim): 273.15
+Sutherland constant (non-dim): 110.4
+Conductivity Model: CONSTANT_PRANDTL 
+Prandtl: 0.72
+Turbulent Conductivity Model: CONSTANT_PRANDTL 
+Turbulent Prandtl: 0.9
+Free-stream static pressure: 71833.4 Pa.
+Free-stream total pressure: 76461.6 Pa.
+Free-stream temperature: 285 K.
+Free-stream total temperature: 290.13 K.
+Free-stream density: 0.878035 kg/m^3.
+Free-stream velocity: (99.3109, 0, 21.1092) m/s. Magnitude: 101.53 m/s.
+Free-stream total energy per unit mass: 209683 m^2/s^2.
+Free-stream viscosity: 1.77406e-05 N.s/m^2.
+Free-stream turb. kinetic energy per unit mass: 13.9161 m^2/s^2.
+Free-stream specific dissipation: 68875.1 1/s.
+-- Reference values:
+Reference specific gas constant: 1 N.m/kg.K.
+Reference pressure: 1 Pa.
+Reference temperature: 1 K.
+Reference density: 1 kg/m^3.
+Reference velocity: 1 m/s.
+Reference energy per unit mass: 1 m^2/s^2.
+Reference viscosity: 1 N.s/m^2.
+Reference conductivity: 1 W/m^2.K.
+-- Resulting non-dimensional state:
+Mach number (non-dim): 0.3
+Reynolds number (non-dim): 8.04e+07. Re length: 16 m.
+Specific gas constant (non-dim): 287.058
+Free-stream temperature (non-dim): 285
+Free-stream pressure (non-dim): 71833.4
+Free-stream density (non-dim): 0.878035
+Free-stream velocity (non-dim): (99.3109, 0, 21.1092). Magnitude: 101.53
+Free-stream total energy per unit mass (non-dim): 209683
+Free-stream viscosity (non-dim): 1.77406e-05
+Free-stream turb. kinetic energy (non-dim): 13.9161
+Free-stream specific dissipation (non-dim): 68875.1
+
+
+Forces breakdown:
+
+Center of Pressure: X=-0.087355Z+33.466161 m.
+
+NOTE: Multiply forces by the non-dimensional factor: 2985038.585495, and the reference factor: 1.000000
+to obtain the dimensional force.
+
+Total CL:       0.523113 | Pressure (  100%):    0.523713 | Friction (    0%):   -0.000600 | Momentum (    0%):    0.000000
+Total CD:       0.064301 | Pressure (   93%):    0.060138 | Friction (    6%):    0.004163 | Momentum (    0%):    0.000000
+Total CSF:     -0.000020 | Pressure (  108%):   -0.000021 | Friction (   -8%):    0.000002 | Momentum (    0%):    0.000000
+Total CL/CD:    8.135425 | Pressure (  107%):    8.708593 | Friction (   -1%):   -0.144214 | Momentum (    0%):    0.000000
+Total CMx:      0.000106 | Pressure (  100%):    0.000106 | Friction (    0%):   -0.000000 | Momentum (    0%):    0.000000
+Total CMy:     -0.669521 | Pressure (   99%):   -0.669343 | Friction (    0%):   -0.000178 | Momentum (    0%):    0.000000
+Total CMz:     -0.000035 | Pressure (  115%):   -0.000041 | Friction (  -15%):    0.000005 | Momentum (    0%):    0.000000
+Total CFx:     -0.045866 | Pressure (  109%):   -0.050063 | Friction (   -9%):    0.004197 | Momentum (    0%):    0.000000
+Total CFy:     -0.000020 | Pressure (  108%):   -0.000021 | Friction (   -8%):    0.000002 | Momentum (    0%):    0.000000
+Total CFz:      0.525051 | Pressure (   99%):    0.524772 | Friction (    0%):    0.000278 | Momentum (    0%):    0.000000
+
+
+Surface name: wall
+
+Total CL    (   99%):    0.523113 | Pressure (  100%):    0.523713 | Friction (    0%):   -0.000600 | Momentum (    0%):    0.000000
+Total CD    (   99%):    0.064301 | Pressure (   93%):    0.060138 | Friction (    6%):    0.004163 | Momentum (    0%):    0.000000
+Total CSF   (  100%):   -0.000020 | Pressure (  108%):   -0.000021 | Friction (   -8%):    0.000002 | Momentum (    0%):    0.000000
+Total CL/CD (  100%):    8.135425 | Pressure (  107%):    8.708593 | Friction (   -1%):   -0.144214 | Momentum (    0%):    0.000000
+Total CMx   (   99%):    0.000106 | Pressure (  100%):    0.000106 | Friction (    0%):   -0.000000 | Momentum (    0%):    0.000000
+Total CMy   (  100%):   -0.669521 | Pressure (   99%):   -0.669343 | Friction (    0%):   -0.000178 | Momentum (    0%):    0.000000
+Total CMz   (  100%):   -0.000035 | Pressure (  115%):   -0.000041 | Friction (  -15%):    0.000005 | Momentum (    0%):    0.000000
+Total CFx   (  100%):   -0.045866 | Pressure (  109%):   -0.050063 | Friction (   -9%):    0.004197 | Momentum (    0%):    0.000000
+Total CFy   (  100%):   -0.000020 | Pressure (  108%):   -0.000021 | Friction (   -8%):    0.000002 | Momentum (    0%):    0.000000
+Total CFz   (   99%):    0.525051 | Pressure (   99%):    0.524772 | Friction (    0%):    0.000278 | Momentum (    0%):    0.000000
+

example/12.0degAOA/surface_and_volume_flow.zip

@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:1e5c4793403c6fc524ec3a1c31e2f8dbfd54d50f38e83cc6b142e72f4d61f7cd
+size 231180167

example/13.0degAOA/config.cfg

@@ -0,0 +1,114 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= RANS
+KIND_TURB_MODEL= SA
+SA_OPTIONS= ROTATION
+RESTART_SOL= NO
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.3
+AOA= 13.0
+FREESTREAM_TEMPERATURE= 285.0
+REYNOLDS_NUMBER= 8.04E7
+REYNOLDS_LENGTH= 16
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 13.063688846316008
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 16
+REF_AREA= 659.6039695925111
+
+% --------------------FLUID MODEL----------------------------------------------%
+%
+FLUID_MODEL= STANDARD_AIR
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.058
+
+% -----------------------VISCOSITY MODEL--------------------------------------%
+%
+VISCOSITY_MODEL= SUTHERLAND
+MU_CONSTANT=1.716e-05
+
+% --------------------------THERMAL MODEL-------------------------------------%
+%
+CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
+PRANDTL_LAM= 0.72
+PRANDTL_TURB= 0.90
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( wall, 0.0 )
+%MARKER_EULER= ( wall )
+MARKER_FAR= ( farfield )
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+FREESTREAM_TURBULENCEINTENSITY= 0.03
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 10.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.2, 1.5, 0.00001, 2000 )
+ITER= 29999
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_ERROR= 1E-7
+LINEAR_SOLVER_ITER= 50
+LINEAR_SOLVER_PREC= ILU
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+MGCYCLE= W_CYCLE
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+MG_DAMP_RESTRICTION= 0.95
+MG_DAMP_PROLONGATION= 0.95
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= JST
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.08
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+MUSCL_TURB= NO
+SLOPE_LIMITER_TURB= VENKATAKRISHNAN
+TIME_DISCRE_TURB= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -6
+CONV_STARTITER= 800
+CONV_FIELD= DRAG
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-5
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= /scratch/users/yrshen/scitec26/geom256samples/020701-1VN.su2
+MESH_FORMAT= SU2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow.dat
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+VOLUME_FILENAME= flow
+SURFACE_FILENAME= surface_flow
+OUTPUT_WRT_FREQ= 200
+WRT_FORCES_BREAKDOWN= YES
+BREAKDOWN_FILENAME= forces_breakdown.dat
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+HISTORY_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+% Change to Tecplot if needed
+VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRIMITIVE, DISSIPATION, MESH_QUALITY)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW, SURFACE_PARAVIEW_ASCII)

example/13.0degAOA/forces_breakdown.dat

@@ -0,0 +1,129 @@
+
+-------------------------------------------------------------------------
+|    ___ _   _ ___                                                      |
+|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
+|   \__ \ |_| |/ /                                                      |
+|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
+|                                                                       |
+-------------------------------------------------------------------------
+| SU2 Project Website: https://su2code.github.io                        |
+|                                                                       |
+| The SU2 Project is maintained by the SU2 Foundation                   |
+| (http://su2foundation.org)                                            |
+-------------------------------------------------------------------------
+| Copyright 2012-2023, SU2 Contributors                                 |
+|                                                                       |
+| SU2 is free software; you can redistribute it and/or                  |
+| modify it under the terms of the GNU Lesser General Public            |
+| License as published by the Free Software Foundation; either          |
+| version 2.1 of the License, or (at your option) any later version.    |
+|                                                                       |
+| SU2 is distributed in the hope that it will be useful,                |
+| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
+| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
+| Lesser General Public License for more details.                       |
+|                                                                       |
+| You should have received a copy of the GNU Lesser General Public      |
+| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
+-------------------------------------------------------------------------
+
+
+Problem definition:
+
+Compressible RANS equations.
+Turbulence model: Spalart Allmaras
+Mach number: 0.3.
+Angle of attack (AoA): 13 deg, and angle of sideslip (AoS): 0 deg.
+Reynolds number: 8.04e+07.
+Dimensional simulation.
+The reference area is 659.604 m^2.
+The reference length is 16 m.
+
+
+Problem definition:
+
+Viscous flow: Computing pressure using the ideal gas law
+based on the free-stream temperature and a density computed
+from the Reynolds number.
+Force coefficients computed using free-stream values.
+-- Input conditions:
+Fluid Model: STANDARD_AIR 
+Specific gas constant: 287.058 N.m/kg.K.
+Specific gas constant (non-dim): 287.058
+Specific Heat Ratio: 1.4000 
+Viscosity Model: SUTHERLAND 
+Ref. Laminar Viscosity: 1.716e-05 N.s/m^2.
+Ref. Temperature: 273.15 K.
+Sutherland Constant: 110.4 K.
+Laminar Viscosity (non-dim): 1.716e-05
+Ref. Temperature (non-dim): 273.15
+Sutherland constant (non-dim): 110.4
+Conductivity Model: CONSTANT_PRANDTL 
+Prandtl: 0.72
+Turbulent Conductivity Model: CONSTANT_PRANDTL 
+Turbulent Prandtl: 0.9
+Free-stream static pressure: 71833.4 Pa.
+Free-stream total pressure: 76461.6 Pa.
+Free-stream temperature: 285 K.
+Free-stream total temperature: 290.13 K.
+Free-stream density: 0.878035 kg/m^3.
+Free-stream velocity: (98.9274, 0, 22.8392) m/s. Magnitude: 101.53 m/s.
+Free-stream total energy per unit mass: 209683 m^2/s^2.
+Free-stream viscosity: 1.77406e-05 N.s/m^2.
+Free-stream turb. kinetic energy per unit mass: 13.9161 m^2/s^2.
+Free-stream specific dissipation: 68875.1 1/s.
+-- Reference values:
+Reference specific gas constant: 1 N.m/kg.K.
+Reference pressure: 1 Pa.
+Reference temperature: 1 K.
+Reference density: 1 kg/m^3.
+Reference velocity: 1 m/s.
+Reference energy per unit mass: 1 m^2/s^2.
+Reference viscosity: 1 N.s/m^2.
+Reference conductivity: 1 W/m^2.K.
+-- Resulting non-dimensional state:
+Mach number (non-dim): 0.3
+Reynolds number (non-dim): 8.04e+07. Re length: 16 m.
+Specific gas constant (non-dim): 287.058
+Free-stream temperature (non-dim): 285
+Free-stream pressure (non-dim): 71833.4
+Free-stream density (non-dim): 0.878035
+Free-stream velocity (non-dim): (98.9274, 0, 22.8392). Magnitude: 101.53
+Free-stream total energy per unit mass (non-dim): 209683
+Free-stream viscosity (non-dim): 1.77406e-05
+Free-stream turb. kinetic energy (non-dim): 13.9161
+Free-stream specific dissipation (non-dim): 68875.1
+
+
+Forces breakdown:
+
+Center of Pressure: X=-0.077479Z+33.666357 m.
+
+NOTE: Multiply forces by the non-dimensional factor: 2985038.585495, and the reference factor: 1.000000
+to obtain the dimensional force.
+
+Total CL:       0.600151 | Pressure (  100%):    0.600854 | Friction (    0%):   -0.000702 | Momentum (    0%):    0.000000
+Total CD:       0.090439 | Pressure (   95%):    0.086477 | Friction (    4%):    0.003962 | Momentum (    0%):    0.000000
+Total CSF:     -0.000029 | Pressure (   94%):   -0.000028 | Friction (    5%):   -0.000002 | Momentum (    0%):    0.000000
+Total CL/CD:    6.635977 | Pressure (  104%):    6.948093 | Friction (   -2%):   -0.177260 | Momentum (    0%):    0.000000
+Total CMx:      0.000099 | Pressure (   99%):    0.000099 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy:     -0.779185 | Pressure (   99%):   -0.779110 | Friction (    0%):   -0.000075 | Momentum (    0%):    0.000000
+Total CMz:     -0.000067 | Pressure (  101%):   -0.000068 | Friction (   -1%):    0.000001 | Momentum (    0%):    0.000000
+Total CFx:     -0.046884 | Pressure (  108%):   -0.050902 | Friction (   -8%):    0.004018 | Momentum (    0%):    0.000000
+Total CFy:     -0.000029 | Pressure (   94%):   -0.000028 | Friction (    5%):   -0.000002 | Momentum (    0%):    0.000000
+Total CFz:      0.605114 | Pressure (   99%):    0.604907 | Friction (    0%):    0.000207 | Momentum (    0%):    0.000000
+
+
+Surface name: wall
+
+Total CL    (   99%):    0.600151 | Pressure (  100%):    0.600854 | Friction (    0%):   -0.000702 | Momentum (    0%):    0.000000
+Total CD    (   99%):    0.090439 | Pressure (   95%):    0.086477 | Friction (    4%):    0.003962 | Momentum (    0%):    0.000000
+Total CSF   (  100%):   -0.000029 | Pressure (   94%):   -0.000028 | Friction (    5%):   -0.000002 | Momentum (    0%):    0.000000
+Total CL/CD (  100%):    6.635977 | Pressure (  104%):    6.948093 | Friction (   -2%):   -0.177260 | Momentum (    0%):    0.000000
+Total CMx   (   99%):    0.000099 | Pressure (   99%):    0.000099 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy   (  100%):   -0.779185 | Pressure (   99%):   -0.779110 | Friction (    0%):   -0.000075 | Momentum (    0%):    0.000000
+Total CMz   (  100%):   -0.000067 | Pressure (  101%):   -0.000068 | Friction (   -1%):    0.000001 | Momentum (    0%):    0.000000
+Total CFx   (  100%):   -0.046884 | Pressure (  108%):   -0.050902 | Friction (   -8%):    0.004018 | Momentum (    0%):    0.000000
+Total CFy   (  100%):   -0.000029 | Pressure (   94%):   -0.000028 | Friction (    5%):   -0.000002 | Momentum (    0%):    0.000000
+Total CFz   (   99%):    0.605114 | Pressure (   99%):    0.604907 | Friction (    0%):    0.000207 | Momentum (    0%):    0.000000
+

example/13.0degAOA/surface_and_volume_flow.zip

@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:b7be2f0cab6376c2925619675fc4628c078188a27aba3e2a7400de8c300917f4
+size 231435218

example/14.0degAOA/config.cfg

@@ -0,0 +1,114 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= RANS
+KIND_TURB_MODEL= SA
+SA_OPTIONS= ROTATION
+RESTART_SOL= NO
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.3
+AOA= 14.0
+FREESTREAM_TEMPERATURE= 285.0
+REYNOLDS_NUMBER= 8.04E7
+REYNOLDS_LENGTH= 16
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 13.063688846316008
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 16
+REF_AREA= 659.6039695925111
+
+% --------------------FLUID MODEL----------------------------------------------%
+%
+FLUID_MODEL= STANDARD_AIR
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.058
+
+% -----------------------VISCOSITY MODEL--------------------------------------%
+%
+VISCOSITY_MODEL= SUTHERLAND
+MU_CONSTANT=1.716e-05
+
+% --------------------------THERMAL MODEL-------------------------------------%
+%
+CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
+PRANDTL_LAM= 0.72
+PRANDTL_TURB= 0.90
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( wall, 0.0 )
+%MARKER_EULER= ( wall )
+MARKER_FAR= ( farfield )
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+FREESTREAM_TURBULENCEINTENSITY= 0.03
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 10.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.2, 1.5, 0.00001, 2000 )
+ITER= 29999
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_ERROR= 1E-7
+LINEAR_SOLVER_ITER= 50
+LINEAR_SOLVER_PREC= ILU
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+MGCYCLE= W_CYCLE
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+MG_DAMP_RESTRICTION= 0.95
+MG_DAMP_PROLONGATION= 0.95
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= JST
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.08
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+MUSCL_TURB= NO
+SLOPE_LIMITER_TURB= VENKATAKRISHNAN
+TIME_DISCRE_TURB= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -6
+CONV_STARTITER= 800
+CONV_FIELD= DRAG
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-5
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= /scratch/users/yrshen/scitec26/geom256samples/020701-1VN.su2
+MESH_FORMAT= SU2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow.dat
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+VOLUME_FILENAME= flow
+SURFACE_FILENAME= surface_flow
+OUTPUT_WRT_FREQ= 200
+WRT_FORCES_BREAKDOWN= YES
+BREAKDOWN_FILENAME= forces_breakdown.dat
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+HISTORY_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+% Change to Tecplot if needed
+VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRIMITIVE, DISSIPATION, MESH_QUALITY)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW, SURFACE_PARAVIEW_ASCII)

example/14.0degAOA/forces_breakdown.dat

@@ -0,0 +1,129 @@
+
+-------------------------------------------------------------------------
+|    ___ _   _ ___                                                      |
+|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
+|   \__ \ |_| |/ /                                                      |
+|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
+|                                                                       |
+-------------------------------------------------------------------------
+| SU2 Project Website: https://su2code.github.io                        |
+|                                                                       |
+| The SU2 Project is maintained by the SU2 Foundation                   |
+| (http://su2foundation.org)                                            |
+-------------------------------------------------------------------------
+| Copyright 2012-2023, SU2 Contributors                                 |
+|                                                                       |
+| SU2 is free software; you can redistribute it and/or                  |
+| modify it under the terms of the GNU Lesser General Public            |
+| License as published by the Free Software Foundation; either          |
+| version 2.1 of the License, or (at your option) any later version.    |
+|                                                                       |
+| SU2 is distributed in the hope that it will be useful,                |
+| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
+| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
+| Lesser General Public License for more details.                       |
+|                                                                       |
+| You should have received a copy of the GNU Lesser General Public      |
+| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
+-------------------------------------------------------------------------
+
+
+Problem definition:
+
+Compressible RANS equations.
+Turbulence model: Spalart Allmaras
+Mach number: 0.3.
+Angle of attack (AoA): 14 deg, and angle of sideslip (AoS): 0 deg.
+Reynolds number: 8.04e+07.
+Dimensional simulation.
+The reference area is 659.604 m^2.
+The reference length is 16 m.
+
+
+Problem definition:
+
+Viscous flow: Computing pressure using the ideal gas law
+based on the free-stream temperature and a density computed
+from the Reynolds number.
+Force coefficients computed using free-stream values.
+-- Input conditions:
+Fluid Model: STANDARD_AIR 
+Specific gas constant: 287.058 N.m/kg.K.
+Specific gas constant (non-dim): 287.058
+Specific Heat Ratio: 1.4000 
+Viscosity Model: SUTHERLAND 
+Ref. Laminar Viscosity: 1.716e-05 N.s/m^2.
+Ref. Temperature: 273.15 K.
+Sutherland Constant: 110.4 K.
+Laminar Viscosity (non-dim): 1.716e-05
+Ref. Temperature (non-dim): 273.15
+Sutherland constant (non-dim): 110.4
+Conductivity Model: CONSTANT_PRANDTL 
+Prandtl: 0.72
+Turbulent Conductivity Model: CONSTANT_PRANDTL 
+Turbulent Prandtl: 0.9
+Free-stream static pressure: 71833.4 Pa.
+Free-stream total pressure: 76461.6 Pa.
+Free-stream temperature: 285 K.
+Free-stream total temperature: 290.13 K.
+Free-stream density: 0.878035 kg/m^3.
+Free-stream velocity: (98.5137, 0, 24.5622) m/s. Magnitude: 101.53 m/s.
+Free-stream total energy per unit mass: 209683 m^2/s^2.
+Free-stream viscosity: 1.77406e-05 N.s/m^2.
+Free-stream turb. kinetic energy per unit mass: 13.9161 m^2/s^2.
+Free-stream specific dissipation: 68875.1 1/s.
+-- Reference values:
+Reference specific gas constant: 1 N.m/kg.K.
+Reference pressure: 1 Pa.
+Reference temperature: 1 K.
+Reference density: 1 kg/m^3.
+Reference velocity: 1 m/s.
+Reference energy per unit mass: 1 m^2/s^2.
+Reference viscosity: 1 N.s/m^2.
+Reference conductivity: 1 W/m^2.K.
+-- Resulting non-dimensional state:
+Mach number (non-dim): 0.3
+Reynolds number (non-dim): 8.04e+07. Re length: 16 m.
+Specific gas constant (non-dim): 287.058
+Free-stream temperature (non-dim): 285
+Free-stream pressure (non-dim): 71833.4
+Free-stream density (non-dim): 0.878035
+Free-stream velocity (non-dim): (98.5137, 0, 24.5622). Magnitude: 101.53
+Free-stream total energy per unit mass (non-dim): 209683
+Free-stream viscosity (non-dim): 1.77406e-05
+Free-stream turb. kinetic energy (non-dim): 13.9161
+Free-stream specific dissipation (non-dim): 68875.1
+
+
+Forces breakdown:
+
+Center of Pressure: X=-0.063874Z+33.876208 m.
+
+NOTE: Multiply forces by the non-dimensional factor: 2985038.585495, and the reference factor: 1.000000
+to obtain the dimensional force.
+
+Total CL:       0.667440 | Pressure (  100%):    0.668253 | Friction (    0%):   -0.000813 | Momentum (    0%):    0.000000
+Total CD:       0.121839 | Pressure (   96%):    0.117850 | Friction (    3%):    0.003989 | Momentum (    0%):    0.000000
+Total CSF:     -0.000022 | Pressure (   97%):   -0.000022 | Friction (    2%):   -0.000001 | Momentum (    0%):    0.000000
+Total CL/CD:    5.478052 | Pressure (  103%):    5.670379 | Friction (   -3%):   -0.203699 | Momentum (    0%):    0.000000
+Total CMx:      0.000009 | Pressure (  101%):    0.000009 | Friction (   -1%):   -0.000000 | Momentum (    0%):    0.000000
+Total CMy:     -0.880746 | Pressure (   99%):   -0.880710 | Friction (    0%):   -0.000036 | Momentum (    0%):    0.000000
+Total CMz:     -0.000052 | Pressure (   94%):   -0.000049 | Friction (    5%):   -0.000003 | Momentum (    0%):    0.000000
+Total CFx:     -0.043249 | Pressure (  109%):   -0.047316 | Friction (   -9%):    0.004067 | Momentum (    0%):    0.000000
+Total CFy:     -0.000022 | Pressure (   97%):   -0.000022 | Friction (    2%):   -0.000001 | Momentum (    0%):    0.000000
+Total CFz:      0.677090 | Pressure (   99%):    0.676913 | Friction (    0%):    0.000177 | Momentum (    0%):    0.000000
+
+
+Surface name: wall
+
+Total CL    (   99%):    0.667440 | Pressure (  100%):    0.668253 | Friction (    0%):   -0.000813 | Momentum (    0%):    0.000000
+Total CD    (   99%):    0.121839 | Pressure (   96%):    0.117850 | Friction (    3%):    0.003989 | Momentum (    0%):    0.000000
+Total CSF   (  100%):   -0.000022 | Pressure (   97%):   -0.000022 | Friction (    2%):   -0.000001 | Momentum (    0%):    0.000000
+Total CL/CD (  100%):    5.478052 | Pressure (  103%):    5.670379 | Friction (   -3%):   -0.203699 | Momentum (    0%):    0.000000
+Total CMx   (   99%):    0.000009 | Pressure (  101%):    0.000009 | Friction (   -1%):   -0.000000 | Momentum (    0%):    0.000000
+Total CMy   (  100%):   -0.880746 | Pressure (   99%):   -0.880710 | Friction (    0%):   -0.000036 | Momentum (    0%):    0.000000
+Total CMz   (  100%):   -0.000052 | Pressure (   94%):   -0.000049 | Friction (    5%):   -0.000003 | Momentum (    0%):    0.000000
+Total CFx   (  100%):   -0.043249 | Pressure (  109%):   -0.047316 | Friction (   -9%):    0.004067 | Momentum (    0%):    0.000000
+Total CFy   (  100%):   -0.000022 | Pressure (   97%):   -0.000022 | Friction (    2%):   -0.000001 | Momentum (    0%):    0.000000
+Total CFz   (   99%):    0.677090 | Pressure (   99%):    0.676913 | Friction (    0%):    0.000177 | Momentum (    0%):    0.000000
+

example/14.0degAOA/surface_and_volume_flow.zip

@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:14f1eda2402886b66874a6816eb3a34ba17f1206f03f666409f2c9e928f90a95
+size 231578797

example/15.0degAOA/config.cfg

@@ -0,0 +1,114 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= RANS
+KIND_TURB_MODEL= SA
+SA_OPTIONS= ROTATION
+RESTART_SOL= NO
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.3
+AOA= 15.0
+FREESTREAM_TEMPERATURE= 285.0
+REYNOLDS_NUMBER= 8.04E7
+REYNOLDS_LENGTH= 16
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 13.063688846316008
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 16
+REF_AREA= 659.6039695925111
+
+% --------------------FLUID MODEL----------------------------------------------%
+%
+FLUID_MODEL= STANDARD_AIR
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.058
+
+% -----------------------VISCOSITY MODEL--------------------------------------%
+%
+VISCOSITY_MODEL= SUTHERLAND
+MU_CONSTANT=1.716e-05
+
+% --------------------------THERMAL MODEL-------------------------------------%
+%
+CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
+PRANDTL_LAM= 0.72
+PRANDTL_TURB= 0.90
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( wall, 0.0 )
+%MARKER_EULER= ( wall )
+MARKER_FAR= ( farfield )
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+FREESTREAM_TURBULENCEINTENSITY= 0.03
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 10.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.2, 1.5, 0.00001, 2000 )
+ITER= 29999
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_ERROR= 1E-7
+LINEAR_SOLVER_ITER= 50
+LINEAR_SOLVER_PREC= ILU
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+MGCYCLE= W_CYCLE
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+MG_DAMP_RESTRICTION= 0.95
+MG_DAMP_PROLONGATION= 0.95
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= JST
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.08
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+MUSCL_TURB= NO
+SLOPE_LIMITER_TURB= VENKATAKRISHNAN
+TIME_DISCRE_TURB= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -6
+CONV_STARTITER= 800
+CONV_FIELD= DRAG
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-5
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= /scratch/users/yrshen/scitec26/geom256samples/020701-1VN.su2
+MESH_FORMAT= SU2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow.dat
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+VOLUME_FILENAME= flow
+SURFACE_FILENAME= surface_flow
+OUTPUT_WRT_FREQ= 200
+WRT_FORCES_BREAKDOWN= YES
+BREAKDOWN_FILENAME= forces_breakdown.dat
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+HISTORY_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+% Change to Tecplot if needed
+VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRIMITIVE, DISSIPATION, MESH_QUALITY)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW, SURFACE_PARAVIEW_ASCII)

example/15.0degAOA/forces_breakdown.dat

@@ -0,0 +1,129 @@
+
+-------------------------------------------------------------------------
+|    ___ _   _ ___                                                      |
+|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
+|   \__ \ |_| |/ /                                                      |
+|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
+|                                                                       |
+-------------------------------------------------------------------------
+| SU2 Project Website: https://su2code.github.io                        |
+|                                                                       |
+| The SU2 Project is maintained by the SU2 Foundation                   |
+| (http://su2foundation.org)                                            |
+-------------------------------------------------------------------------
+| Copyright 2012-2023, SU2 Contributors                                 |
+|                                                                       |
+| SU2 is free software; you can redistribute it and/or                  |
+| modify it under the terms of the GNU Lesser General Public            |
+| License as published by the Free Software Foundation; either          |
+| version 2.1 of the License, or (at your option) any later version.    |
+|                                                                       |
+| SU2 is distributed in the hope that it will be useful,                |
+| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
+| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
+| Lesser General Public License for more details.                       |
+|                                                                       |
+| You should have received a copy of the GNU Lesser General Public      |
+| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
+-------------------------------------------------------------------------
+
+
+Problem definition:
+
+Compressible RANS equations.
+Turbulence model: Spalart Allmaras
+Mach number: 0.3.
+Angle of attack (AoA): 15 deg, and angle of sideslip (AoS): 0 deg.
+Reynolds number: 8.04e+07.
+Dimensional simulation.
+The reference area is 659.604 m^2.
+The reference length is 16 m.
+
+
+Problem definition:
+
+Viscous flow: Computing pressure using the ideal gas law
+based on the free-stream temperature and a density computed
+from the Reynolds number.
+Force coefficients computed using free-stream values.
+-- Input conditions:
+Fluid Model: STANDARD_AIR 
+Specific gas constant: 287.058 N.m/kg.K.
+Specific gas constant (non-dim): 287.058
+Specific Heat Ratio: 1.4000 
+Viscosity Model: SUTHERLAND 
+Ref. Laminar Viscosity: 1.716e-05 N.s/m^2.
+Ref. Temperature: 273.15 K.
+Sutherland Constant: 110.4 K.
+Laminar Viscosity (non-dim): 1.716e-05
+Ref. Temperature (non-dim): 273.15
+Sutherland constant (non-dim): 110.4
+Conductivity Model: CONSTANT_PRANDTL 
+Prandtl: 0.72
+Turbulent Conductivity Model: CONSTANT_PRANDTL 
+Turbulent Prandtl: 0.9
+Free-stream static pressure: 71833.4 Pa.
+Free-stream total pressure: 76461.6 Pa.
+Free-stream temperature: 285 K.
+Free-stream total temperature: 290.13 K.
+Free-stream density: 0.878035 kg/m^3.
+Free-stream velocity: (98.07, 0, 26.2778) m/s. Magnitude: 101.53 m/s.
+Free-stream total energy per unit mass: 209683 m^2/s^2.
+Free-stream viscosity: 1.77406e-05 N.s/m^2.
+Free-stream turb. kinetic energy per unit mass: 13.9161 m^2/s^2.
+Free-stream specific dissipation: 68875.1 1/s.
+-- Reference values:
+Reference specific gas constant: 1 N.m/kg.K.
+Reference pressure: 1 Pa.
+Reference temperature: 1 K.
+Reference density: 1 kg/m^3.
+Reference velocity: 1 m/s.
+Reference energy per unit mass: 1 m^2/s^2.
+Reference viscosity: 1 N.s/m^2.
+Reference conductivity: 1 W/m^2.K.
+-- Resulting non-dimensional state:
+Mach number (non-dim): 0.3
+Reynolds number (non-dim): 8.04e+07. Re length: 16 m.
+Specific gas constant (non-dim): 287.058
+Free-stream temperature (non-dim): 285
+Free-stream pressure (non-dim): 71833.4
+Free-stream density (non-dim): 0.878035
+Free-stream velocity (non-dim): (98.07, 0, 26.2778). Magnitude: 101.53
+Free-stream total energy per unit mass (non-dim): 209683
+Free-stream viscosity (non-dim): 1.77406e-05
+Free-stream turb. kinetic energy (non-dim): 13.9161
+Free-stream specific dissipation (non-dim): 68875.1
+
+
+Forces breakdown:
+
+Center of Pressure: X=-0.055198Z+34.045600 m.
+
+NOTE: Multiply forces by the non-dimensional factor: 2985038.585495, and the reference factor: 1.000000
+to obtain the dimensional force.
+
+Total CL:       0.722323 | Pressure (  100%):    0.723237 | Friction (    0%):   -0.000914 | Momentum (    0%):    0.000000
+Total CD:       0.151435 | Pressure (   97%):    0.147380 | Friction (    2%):    0.004055 | Momentum (    0%):    0.000000
+Total CSF:     -0.000056 | Pressure (  105%):   -0.000059 | Friction (   -5%):    0.000003 | Momentum (    0%):    0.000000
+Total CL/CD:    4.769855 | Pressure (  102%):    4.907291 | Friction (   -4%):   -0.225488 | Momentum (    0%):    0.000000
+Total CMx:     -0.000082 | Pressure (  100%):   -0.000082 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy:     -0.966354 | Pressure (   99%):   -0.966330 | Friction (    0%):   -0.000025 | Momentum (    0%):    0.000000
+Total CMz:     -0.000126 | Pressure (  102%):   -0.000129 | Friction (   -2%):    0.000004 | Momentum (    0%):    0.000000
+Total CFx:     -0.040676 | Pressure (  110%):   -0.044829 | Friction (  -10%):    0.004153 | Momentum (    0%):    0.000000
+Total CFy:     -0.000056 | Pressure (  105%):   -0.000059 | Friction (   -5%):    0.000003 | Momentum (    0%):    0.000000
+Total CFz:      0.736905 | Pressure (   99%):    0.736738 | Friction (    0%):    0.000166 | Momentum (    0%):    0.000000
+
+
+Surface name: wall
+
+Total CL    (   99%):    0.722323 | Pressure (  100%):    0.723237 | Friction (    0%):   -0.000914 | Momentum (    0%):    0.000000
+Total CD    (   99%):    0.151435 | Pressure (   97%):    0.147380 | Friction (    2%):    0.004055 | Momentum (    0%):    0.000000
+Total CSF   (  100%):   -0.000056 | Pressure (  105%):   -0.000059 | Friction (   -5%):    0.000003 | Momentum (    0%):    0.000000
+Total CL/CD (  100%):    4.769855 | Pressure (  102%):    4.907291 | Friction (   -4%):   -0.225488 | Momentum (    0%):    0.000000
+Total CMx   (  100%):   -0.000082 | Pressure (  100%):   -0.000082 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy   (  100%):   -0.966354 | Pressure (   99%):   -0.966330 | Friction (    0%):   -0.000025 | Momentum (    0%):    0.000000
+Total CMz   (  100%):   -0.000126 | Pressure (  102%):   -0.000129 | Friction (   -2%):    0.000004 | Momentum (    0%):    0.000000
+Total CFx   (  100%):   -0.040676 | Pressure (  110%):   -0.044829 | Friction (  -10%):    0.004153 | Momentum (    0%):    0.000000
+Total CFy   (  100%):   -0.000056 | Pressure (  105%):   -0.000059 | Friction (   -5%):    0.000003 | Momentum (    0%):    0.000000
+Total CFz   (   99%):    0.736905 | Pressure (   99%):    0.736738 | Friction (    0%):    0.000166 | Momentum (    0%):    0.000000
+

example/15.0degAOA/surface_and_volume_flow.zip

@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:27a50c24af7a8fce61a67d693d9ef673f1bc1084c327524c5a1ada9d85a5a8a1
+size 231633566

example/16.0degAOA/config.cfg

@@ -0,0 +1,114 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= RANS
+KIND_TURB_MODEL= SA
+SA_OPTIONS= ROTATION
+RESTART_SOL= NO
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.3
+AOA= 16.0
+FREESTREAM_TEMPERATURE= 285.0
+REYNOLDS_NUMBER= 8.04E7
+REYNOLDS_LENGTH= 16
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 13.063688846316008
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 16
+REF_AREA= 659.6039695925111
+
+% --------------------FLUID MODEL----------------------------------------------%
+%
+FLUID_MODEL= STANDARD_AIR
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.058
+
+% -----------------------VISCOSITY MODEL--------------------------------------%
+%
+VISCOSITY_MODEL= SUTHERLAND
+MU_CONSTANT=1.716e-05
+
+% --------------------------THERMAL MODEL-------------------------------------%
+%
+CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
+PRANDTL_LAM= 0.72
+PRANDTL_TURB= 0.90
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( wall, 0.0 )
+%MARKER_EULER= ( wall )
+MARKER_FAR= ( farfield )
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+FREESTREAM_TURBULENCEINTENSITY= 0.03
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 10.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.2, 1.5, 0.00001, 2000 )
+ITER= 29999
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_ERROR= 1E-7
+LINEAR_SOLVER_ITER= 50
+LINEAR_SOLVER_PREC= ILU
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+MGCYCLE= W_CYCLE
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+MG_DAMP_RESTRICTION= 0.95
+MG_DAMP_PROLONGATION= 0.95
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= JST
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.08
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+MUSCL_TURB= NO
+SLOPE_LIMITER_TURB= VENKATAKRISHNAN
+TIME_DISCRE_TURB= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -6
+CONV_STARTITER= 800
+CONV_FIELD= DRAG
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-5
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= /scratch/users/yrshen/scitec26/geom256samples/020701-1VN.su2
+MESH_FORMAT= SU2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow.dat
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+VOLUME_FILENAME= flow
+SURFACE_FILENAME= surface_flow
+OUTPUT_WRT_FREQ= 200
+WRT_FORCES_BREAKDOWN= YES
+BREAKDOWN_FILENAME= forces_breakdown.dat
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+HISTORY_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+% Change to Tecplot if needed
+VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRIMITIVE, DISSIPATION, MESH_QUALITY)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW, SURFACE_PARAVIEW_ASCII)

example/16.0degAOA/forces_breakdown.dat

@@ -0,0 +1,129 @@
+
+-------------------------------------------------------------------------
+|    ___ _   _ ___                                                      |
+|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
+|   \__ \ |_| |/ /                                                      |
+|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
+|                                                                       |
+-------------------------------------------------------------------------
+| SU2 Project Website: https://su2code.github.io                        |
+|                                                                       |
+| The SU2 Project is maintained by the SU2 Foundation                   |
+| (http://su2foundation.org)                                            |
+-------------------------------------------------------------------------
+| Copyright 2012-2023, SU2 Contributors                                 |
+|                                                                       |
+| SU2 is free software; you can redistribute it and/or                  |
+| modify it under the terms of the GNU Lesser General Public            |
+| License as published by the Free Software Foundation; either          |
+| version 2.1 of the License, or (at your option) any later version.    |
+|                                                                       |
+| SU2 is distributed in the hope that it will be useful,                |
+| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
+| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
+| Lesser General Public License for more details.                       |
+|                                                                       |
+| You should have received a copy of the GNU Lesser General Public      |
+| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
+-------------------------------------------------------------------------
+
+
+Problem definition:
+
+Compressible RANS equations.
+Turbulence model: Spalart Allmaras
+Mach number: 0.3.
+Angle of attack (AoA): 16 deg, and angle of sideslip (AoS): 0 deg.
+Reynolds number: 8.04e+07.
+Dimensional simulation.
+The reference area is 659.604 m^2.
+The reference length is 16 m.
+
+
+Problem definition:
+
+Viscous flow: Computing pressure using the ideal gas law
+based on the free-stream temperature and a density computed
+from the Reynolds number.
+Force coefficients computed using free-stream values.
+-- Input conditions:
+Fluid Model: STANDARD_AIR 
+Specific gas constant: 287.058 N.m/kg.K.
+Specific gas constant (non-dim): 287.058
+Specific Heat Ratio: 1.4000 
+Viscosity Model: SUTHERLAND 
+Ref. Laminar Viscosity: 1.716e-05 N.s/m^2.
+Ref. Temperature: 273.15 K.
+Sutherland Constant: 110.4 K.
+Laminar Viscosity (non-dim): 1.716e-05
+Ref. Temperature (non-dim): 273.15
+Sutherland constant (non-dim): 110.4
+Conductivity Model: CONSTANT_PRANDTL 
+Prandtl: 0.72
+Turbulent Conductivity Model: CONSTANT_PRANDTL 
+Turbulent Prandtl: 0.9
+Free-stream static pressure: 71833.4 Pa.
+Free-stream total pressure: 76461.6 Pa.
+Free-stream temperature: 285 K.
+Free-stream total temperature: 290.13 K.
+Free-stream density: 0.878035 kg/m^3.
+Free-stream velocity: (97.5965, 0, 27.9853) m/s. Magnitude: 101.53 m/s.
+Free-stream total energy per unit mass: 209683 m^2/s^2.
+Free-stream viscosity: 1.77406e-05 N.s/m^2.
+Free-stream turb. kinetic energy per unit mass: 13.9161 m^2/s^2.
+Free-stream specific dissipation: 68875.1 1/s.
+-- Reference values:
+Reference specific gas constant: 1 N.m/kg.K.
+Reference pressure: 1 Pa.
+Reference temperature: 1 K.
+Reference density: 1 kg/m^3.
+Reference velocity: 1 m/s.
+Reference energy per unit mass: 1 m^2/s^2.
+Reference viscosity: 1 N.s/m^2.
+Reference conductivity: 1 W/m^2.K.
+-- Resulting non-dimensional state:
+Mach number (non-dim): 0.3
+Reynolds number (non-dim): 8.04e+07. Re length: 16 m.
+Specific gas constant (non-dim): 287.058
+Free-stream temperature (non-dim): 285
+Free-stream pressure (non-dim): 71833.4
+Free-stream density (non-dim): 0.878035
+Free-stream velocity (non-dim): (97.5965, 0, 27.9853). Magnitude: 101.53
+Free-stream total energy per unit mass (non-dim): 209683
+Free-stream viscosity (non-dim): 1.77406e-05
+Free-stream turb. kinetic energy (non-dim): 13.9161
+Free-stream specific dissipation (non-dim): 68875.1
+
+
+Forces breakdown:
+
+Center of Pressure: X=-0.047963Z+34.249514 m.
+
+NOTE: Multiply forces by the non-dimensional factor: 2985038.585495, and the reference factor: 1.000000
+to obtain the dimensional force.
+
+Total CL:       0.773699 | Pressure (  100%):    0.774669 | Friction (    0%):   -0.000970 | Momentum (    0%):    0.000000
+Total CD:       0.182239 | Pressure (   97%):    0.178246 | Friction (    2%):    0.003993 | Momentum (    0%):    0.000000
+Total CSF:     -0.000116 | Pressure (   99%):   -0.000115 | Friction (    0%):   -0.000001 | Momentum (    0%):    0.000000
+Total CL/CD:    4.245515 | Pressure (  102%):    4.346076 | Friction (   -5%):   -0.242981 | Momentum (    0%):    0.000000
+Total CMx:     -0.000372 | Pressure (  100%):   -0.000373 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy:     -1.051292 | Pressure (   99%):   -1.051259 | Friction (    0%):   -0.000033 | Momentum (    0%):    0.000000
+Total CMz:     -0.000212 | Pressure (  100%):   -0.000212 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CFx:     -0.038081 | Pressure (  110%):   -0.042187 | Friction (  -10%):    0.004106 | Momentum (    0%):    0.000000
+Total CFy:     -0.000116 | Pressure (   99%):   -0.000115 | Friction (    0%):   -0.000001 | Momentum (    0%):    0.000000
+Total CFz:      0.793959 | Pressure (   99%):    0.793791 | Friction (    0%):    0.000168 | Momentum (    0%):    0.000000
+
+
+Surface name: wall
+
+Total CL    (   99%):    0.773699 | Pressure (  100%):    0.774669 | Friction (    0%):   -0.000970 | Momentum (    0%):    0.000000
+Total CD    (   99%):    0.182239 | Pressure (   97%):    0.178246 | Friction (    2%):    0.003993 | Momentum (    0%):    0.000000
+Total CSF   (  100%):   -0.000116 | Pressure (   99%):   -0.000115 | Friction (    0%):   -0.000001 | Momentum (    0%):    0.000000
+Total CL/CD (  100%):    4.245515 | Pressure (  102%):    4.346076 | Friction (   -5%):   -0.242981 | Momentum (    0%):    0.000000
+Total CMx   (  100%):   -0.000372 | Pressure (  100%):   -0.000373 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy   (  100%):   -1.051292 | Pressure (   99%):   -1.051259 | Friction (    0%):   -0.000033 | Momentum (    0%):    0.000000
+Total CMz   (  100%):   -0.000212 | Pressure (  100%):   -0.000212 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CFx   (  100%):   -0.038081 | Pressure (  110%):   -0.042187 | Friction (  -10%):    0.004106 | Momentum (    0%):    0.000000
+Total CFy   (  100%):   -0.000116 | Pressure (   99%):   -0.000115 | Friction (    0%):   -0.000001 | Momentum (    0%):    0.000000
+Total CFz   (   99%):    0.793959 | Pressure (   99%):    0.793791 | Friction (    0%):    0.000168 | Momentum (    0%):    0.000000
+

example/16.0degAOA/surface_and_volume_flow.zip

@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:0085f43c3ff76600f11c2f8de23dd295957d0ed7b576515e87066dbbd0c70276
+size 231632254

example/17.0degAOA/config.cfg

@@ -0,0 +1,114 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= RANS
+KIND_TURB_MODEL= SA
+SA_OPTIONS= ROTATION
+RESTART_SOL= NO
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.3
+AOA= 17.0
+FREESTREAM_TEMPERATURE= 285.0
+REYNOLDS_NUMBER= 8.04E7
+REYNOLDS_LENGTH= 16
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 13.063688846316008
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 16
+REF_AREA= 659.6039695925111
+
+% --------------------FLUID MODEL----------------------------------------------%
+%
+FLUID_MODEL= STANDARD_AIR
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.058
+
+% -----------------------VISCOSITY MODEL--------------------------------------%
+%
+VISCOSITY_MODEL= SUTHERLAND
+MU_CONSTANT=1.716e-05
+
+% --------------------------THERMAL MODEL-------------------------------------%
+%
+CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
+PRANDTL_LAM= 0.72
+PRANDTL_TURB= 0.90
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( wall, 0.0 )
+%MARKER_EULER= ( wall )
+MARKER_FAR= ( farfield )
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+FREESTREAM_TURBULENCEINTENSITY= 0.03
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 10.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.2, 1.5, 0.00001, 2000 )
+ITER= 29999
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_ERROR= 1E-7
+LINEAR_SOLVER_ITER= 50
+LINEAR_SOLVER_PREC= ILU
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+MGCYCLE= W_CYCLE
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+MG_DAMP_RESTRICTION= 0.95
+MG_DAMP_PROLONGATION= 0.95
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= JST
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.08
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+MUSCL_TURB= NO
+SLOPE_LIMITER_TURB= VENKATAKRISHNAN
+TIME_DISCRE_TURB= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -6
+CONV_STARTITER= 800
+CONV_FIELD= DRAG
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-5
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= /scratch/users/yrshen/scitec26/geom256samples/020701-1VN.su2
+MESH_FORMAT= SU2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow.dat
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+VOLUME_FILENAME= flow
+SURFACE_FILENAME= surface_flow
+OUTPUT_WRT_FREQ= 200
+WRT_FORCES_BREAKDOWN= YES
+BREAKDOWN_FILENAME= forces_breakdown.dat
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+HISTORY_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+% Change to Tecplot if needed
+VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRIMITIVE, DISSIPATION, MESH_QUALITY)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW, SURFACE_PARAVIEW_ASCII)

example/17.0degAOA/forces_breakdown.dat

@@ -0,0 +1,129 @@
+
+-------------------------------------------------------------------------
+|    ___ _   _ ___                                                      |
+|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
+|   \__ \ |_| |/ /                                                      |
+|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
+|                                                                       |
+-------------------------------------------------------------------------
+| SU2 Project Website: https://su2code.github.io                        |
+|                                                                       |
+| The SU2 Project is maintained by the SU2 Foundation                   |
+| (http://su2foundation.org)                                            |
+-------------------------------------------------------------------------
+| Copyright 2012-2023, SU2 Contributors                                 |
+|                                                                       |
+| SU2 is free software; you can redistribute it and/or                  |
+| modify it under the terms of the GNU Lesser General Public            |
+| License as published by the Free Software Foundation; either          |
+| version 2.1 of the License, or (at your option) any later version.    |
+|                                                                       |
+| SU2 is distributed in the hope that it will be useful,                |
+| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
+| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
+| Lesser General Public License for more details.                       |
+|                                                                       |
+| You should have received a copy of the GNU Lesser General Public      |
+| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
+-------------------------------------------------------------------------
+
+
+Problem definition:
+
+Compressible RANS equations.
+Turbulence model: Spalart Allmaras
+Mach number: 0.3.
+Angle of attack (AoA): 17 deg, and angle of sideslip (AoS): 0 deg.
+Reynolds number: 8.04e+07.
+Dimensional simulation.
+The reference area is 659.604 m^2.
+The reference length is 16 m.
+
+
+Problem definition:
+
+Viscous flow: Computing pressure using the ideal gas law
+based on the free-stream temperature and a density computed
+from the Reynolds number.
+Force coefficients computed using free-stream values.
+-- Input conditions:
+Fluid Model: STANDARD_AIR 
+Specific gas constant: 287.058 N.m/kg.K.
+Specific gas constant (non-dim): 287.058
+Specific Heat Ratio: 1.4000 
+Viscosity Model: SUTHERLAND 
+Ref. Laminar Viscosity: 1.716e-05 N.s/m^2.
+Ref. Temperature: 273.15 K.
+Sutherland Constant: 110.4 K.
+Laminar Viscosity (non-dim): 1.716e-05
+Ref. Temperature (non-dim): 273.15
+Sutherland constant (non-dim): 110.4
+Conductivity Model: CONSTANT_PRANDTL 
+Prandtl: 0.72
+Turbulent Conductivity Model: CONSTANT_PRANDTL 
+Turbulent Prandtl: 0.9
+Free-stream static pressure: 71833.4 Pa.
+Free-stream total pressure: 76461.6 Pa.
+Free-stream temperature: 285 K.
+Free-stream total temperature: 290.13 K.
+Free-stream density: 0.878035 kg/m^3.
+Free-stream velocity: (97.0932, 0, 29.6844) m/s. Magnitude: 101.53 m/s.
+Free-stream total energy per unit mass: 209683 m^2/s^2.
+Free-stream viscosity: 1.77406e-05 N.s/m^2.
+Free-stream turb. kinetic energy per unit mass: 13.9161 m^2/s^2.
+Free-stream specific dissipation: 68875.1 1/s.
+-- Reference values:
+Reference specific gas constant: 1 N.m/kg.K.
+Reference pressure: 1 Pa.
+Reference temperature: 1 K.
+Reference density: 1 kg/m^3.
+Reference velocity: 1 m/s.
+Reference energy per unit mass: 1 m^2/s^2.
+Reference viscosity: 1 N.s/m^2.
+Reference conductivity: 1 W/m^2.K.
+-- Resulting non-dimensional state:
+Mach number (non-dim): 0.3
+Reynolds number (non-dim): 8.04e+07. Re length: 16 m.
+Specific gas constant (non-dim): 287.058
+Free-stream temperature (non-dim): 285
+Free-stream pressure (non-dim): 71833.4
+Free-stream density (non-dim): 0.878035
+Free-stream velocity (non-dim): (97.0932, 0, 29.6844). Magnitude: 101.53
+Free-stream total energy per unit mass (non-dim): 209683
+Free-stream viscosity (non-dim): 1.77406e-05
+Free-stream turb. kinetic energy (non-dim): 13.9161
+Free-stream specific dissipation (non-dim): 68875.1
+
+
+Forces breakdown:
+
+Center of Pressure: X=-0.041399Z+34.427272 m.
+
+NOTE: Multiply forces by the non-dimensional factor: 2985038.585495, and the reference factor: 1.000000
+to obtain the dimensional force.
+
+Total CL:       0.819467 | Pressure (  100%):    0.820493 | Friction (    0%):   -0.001026 | Momentum (    0%):    0.000000
+Total CD:       0.213904 | Pressure (   98%):    0.209968 | Friction (    1%):    0.003936 | Momentum (    0%):    0.000000
+Total CSF:      0.000058 | Pressure (  105%):    0.000062 | Friction (   -5%):   -0.000003 | Momentum (    0%):    0.000000
+Total CL/CD:    3.831008 | Pressure (  102%):    3.907702 | Friction (   -6%):   -0.260744 | Momentum (    0%):    0.000000
+Total CMx:     -0.000393 | Pressure (  100%):   -0.000393 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy:     -1.129866 | Pressure (   99%):   -1.129825 | Friction (    0%):   -0.000041 | Momentum (    0%):    0.000000
+Total CMz:      0.000078 | Pressure (  103%):    0.000081 | Friction (   -3%):   -0.000003 | Momentum (    0%):    0.000000
+Total CFx:     -0.035032 | Pressure (  111%):   -0.039095 | Friction (  -11%):    0.004064 | Momentum (    0%):    0.000000
+Total CFy:      0.000058 | Pressure (  105%):    0.000062 | Friction (   -5%):   -0.000003 | Momentum (    0%):    0.000000
+Total CFz:      0.846200 | Pressure (   99%):    0.846031 | Friction (    0%):    0.000169 | Momentum (    0%):    0.000000
+
+
+Surface name: wall
+
+Total CL    (   99%):    0.819467 | Pressure (  100%):    0.820493 | Friction (    0%):   -0.001026 | Momentum (    0%):    0.000000
+Total CD    (   99%):    0.213904 | Pressure (   98%):    0.209968 | Friction (    1%):    0.003936 | Momentum (    0%):    0.000000
+Total CSF   (   99%):    0.000058 | Pressure (  105%):    0.000062 | Friction (   -5%):   -0.000003 | Momentum (    0%):    0.000000
+Total CL/CD (  100%):    3.831008 | Pressure (  102%):    3.907702 | Friction (   -6%):   -0.260744 | Momentum (    0%):    0.000000
+Total CMx   (  100%):   -0.000393 | Pressure (  100%):   -0.000393 | Friction (    0%):    0.000000 | Momentum (    0%):    0.000000
+Total CMy   (  100%):   -1.129866 | Pressure (   99%):   -1.129825 | Friction (    0%):   -0.000041 | Momentum (    0%):    0.000000
+Total CMz   (   99%):    0.000078 | Pressure (  103%):    0.000081 | Friction (   -3%):   -0.000003 | Momentum (    0%):    0.000000
+Total CFx   (  100%):   -0.035032 | Pressure (  111%):   -0.039095 | Friction (  -11%):    0.004064 | Momentum (    0%):    0.000000
+Total CFy   (   99%):    0.000058 | Pressure (  105%):    0.000062 | Friction (   -5%):   -0.000003 | Momentum (    0%):    0.000000
+Total CFz   (   99%):    0.846200 | Pressure (   99%):    0.846031 | Friction (    0%):    0.000169 | Momentum (    0%):    0.000000
+

example/17.0degAOA/surface_and_volume_flow.zip

@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:7b1968d5e26c4ddfce6b08f4acff414c6a718ecf642deeafbde88b53e1199d0d
+size 231623259

example/18.0degAOA/config.cfg

@@ -0,0 +1,114 @@
+% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
+SOLVER= RANS
+KIND_TURB_MODEL= SA
+SA_OPTIONS= ROTATION
+RESTART_SOL= NO
+
+% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
+%
+MACH_NUMBER= 0.3
+AOA= 18.0
+FREESTREAM_TEMPERATURE= 285.0
+REYNOLDS_NUMBER= 8.04E7
+REYNOLDS_LENGTH= 16
+
+% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_ORIGIN_MOMENT_X = 13.063688846316008
+REF_ORIGIN_MOMENT_Y = 0.00
+REF_ORIGIN_MOMENT_Z = 0.00
+REF_LENGTH= 16
+REF_AREA= 659.6039695925111
+
+% --------------------FLUID MODEL----------------------------------------------%
+%
+FLUID_MODEL= STANDARD_AIR
+GAMMA_VALUE= 1.4
+GAS_CONSTANT= 287.058
+
+% -----------------------VISCOSITY MODEL--------------------------------------%
+%
+VISCOSITY_MODEL= SUTHERLAND
+MU_CONSTANT=1.716e-05
+
+% --------------------------THERMAL MODEL-------------------------------------%
+%
+CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
+PRANDTL_LAM= 0.72
+PRANDTL_TURB= 0.90
+
+% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
+MARKER_HEATFLUX= ( wall, 0.0 )
+%MARKER_EULER= ( wall )
+MARKER_FAR= ( farfield )
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
+FREESTREAM_TURBULENCEINTENSITY= 0.03
+
+% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
+NUM_METHOD_GRAD= GREEN_GAUSS
+CFL_NUMBER= 10.0
+CFL_ADAPT= YES
+CFL_ADAPT_PARAM= ( 0.2, 1.5, 0.00001, 2000 )
+ITER= 29999
+LINEAR_SOLVER= FGMRES
+LINEAR_SOLVER_ERROR= 1E-7
+LINEAR_SOLVER_ITER= 50
+LINEAR_SOLVER_PREC= ILU
+
+% -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
+MGLEVEL= 0
+MGCYCLE= W_CYCLE
+MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
+MG_POST_SMOOTH= ( 0, 0, 0, 0 )
+MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
+MG_DAMP_RESTRICTION= 0.95
+MG_DAMP_PROLONGATION= 0.95
+
+% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
+CONV_NUM_METHOD_FLOW= JST
+MUSCL_FLOW= NO
+SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
+VENKAT_LIMITER_COEFF= 0.08
+JST_SENSOR_COEFF= ( 0.5, 0.02 )
+TIME_DISCRE_FLOW= EULER_IMPLICIT
+
+% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
+CONV_NUM_METHOD_TURB= SCALAR_UPWIND
+MUSCL_TURB= NO
+SLOPE_LIMITER_TURB= VENKATAKRISHNAN
+TIME_DISCRE_TURB= EULER_IMPLICIT
+
+% --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
+CONV_RESIDUAL_MINVAL= -6
+CONV_STARTITER= 800
+CONV_FIELD= DRAG
+CONV_CAUCHY_ELEMS= 100
+CONV_CAUCHY_EPS= 1E-5
+
+% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
+%
+MESH_FILENAME= /scratch/users/yrshen/scitec26/geom256samples/020701-1VN.su2
+MESH_FORMAT= SU2
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow.dat
+TABULAR_FORMAT= CSV
+CONV_FILENAME= history
+RESTART_FILENAME= restart_flow.dat
+VOLUME_FILENAME= flow
+SURFACE_FILENAME= surface_flow
+OUTPUT_WRT_FREQ= 200
+WRT_FORCES_BREAKDOWN= YES
+BREAKDOWN_FILENAME= forces_breakdown.dat
+SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+HISTORY_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_NU_TILDE, LIFT, DRAG, CFL_NUMBER, LINSOL, CAUCHY)
+% Change to Tecplot if needed
+VOLUME_OUTPUT= (COORDINATES, SOLUTION, PRIMITIVE, DISSIPATION, MESH_QUALITY)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW, SURFACE_PARAVIEW_ASCII)

example/18.0degAOA/forces_breakdown.dat

@@ -0,0 +1,129 @@
+
+-------------------------------------------------------------------------
+|    ___ _   _ ___                                                      |
+|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
+|   \__ \ |_| |/ /                                                      |
+|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
+|                                                                       |
+-------------------------------------------------------------------------
+| SU2 Project Website: https://su2code.github.io                        |
+|                                                                       |
+| The SU2 Project is maintained by the SU2 Foundation                   |
+| (http://su2foundation.org)                                            |
+-------------------------------------------------------------------------
+| Copyright 2012-2023, SU2 Contributors                                 |
+|                                                                       |
+| SU2 is free software; you can redistribute it and/or                  |
+| modify it under the terms of the GNU Lesser General Public            |
+| License as published by the Free Software Foundation; either          |
+| version 2.1 of the License, or (at your option) any later version.    |
+|                                                                       |
+| SU2 is distributed in the hope that it will be useful,                |
+| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
+| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
+| Lesser General Public License for more details.                       |
+|                                                                       |
+| You should have received a copy of the GNU Lesser General Public      |
+| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
+-------------------------------------------------------------------------
+
+
+Problem definition:
+
+Compressible RANS equations.
+Turbulence model: Spalart Allmaras
+Mach number: 0.3.
+Angle of attack (AoA): 18 deg, and angle of sideslip (AoS): 0 deg.
+Reynolds number: 8.04e+07.
+Dimensional simulation.
+The reference area is 659.604 m^2.
+The reference length is 16 m.
+
+
+Problem definition:
+
+Viscous flow: Computing pressure using the ideal gas law
+based on the free-stream temperature and a density computed
+from the Reynolds number.
+Force coefficients computed using free-stream values.
+-- Input conditions:
+Fluid Model: STANDARD_AIR 
+Specific gas constant: 287.058 N.m/kg.K.
+Specific gas constant (non-dim): 287.058
+Specific Heat Ratio: 1.4000 
+Viscosity Model: SUTHERLAND 
+Ref. Laminar Viscosity: 1.716e-05 N.s/m^2.
+Ref. Temperature: 273.15 K.
+Sutherland Constant: 110.4 K.
+Laminar Viscosity (non-dim): 1.716e-05
+Ref. Temperature (non-dim): 273.15
+Sutherland constant (non-dim): 110.4
+Conductivity Model: CONSTANT_PRANDTL 
+Prandtl: 0.72
+Turbulent Conductivity Model: CONSTANT_PRANDTL 
+Turbulent Prandtl: 0.9
+Free-stream static pressure: 71833.4 Pa.
+Free-stream total pressure: 76461.6 Pa.
+Free-stream temperature: 285 K.
+Free-stream total temperature: 290.13 K.
+Free-stream density: 0.878035 kg/m^3.
+Free-stream velocity: (96.5604, 0, 31.3744) m/s. Magnitude: 101.53 m/s.
+Free-stream total energy per unit mass: 209683 m^2/s^2.
+Free-stream viscosity: 1.77406e-05 N.s/m^2.
+Free-stream turb. kinetic energy per unit mass: 13.9161 m^2/s^2.
+Free-stream specific dissipation: 68875.1 1/s.
+-- Reference values:
+Reference specific gas constant: 1 N.m/kg.K.
+Reference pressure: 1 Pa.
+Reference temperature: 1 K.
+Reference density: 1 kg/m^3.
+Reference velocity: 1 m/s.
+Reference energy per unit mass: 1 m^2/s^2.
+Reference viscosity: 1 N.s/m^2.
+Reference conductivity: 1 W/m^2.K.
+-- Resulting non-dimensional state:
+Mach number (non-dim): 0.3
+Reynolds number (non-dim): 8.04e+07. Re length: 16 m.
+Specific gas constant (non-dim): 287.058
+Free-stream temperature (non-dim): 285
+Free-stream pressure (non-dim): 71833.4
+Free-stream density (non-dim): 0.878035
+Free-stream velocity (non-dim): (96.5604, 0, 31.3744). Magnitude: 101.53
+Free-stream total energy per unit mass (non-dim): 209683
+Free-stream viscosity (non-dim): 1.77406e-05
+Free-stream turb. kinetic energy (non-dim): 13.9161
+Free-stream specific dissipation (non-dim): 68875.1
+
+
+Forces breakdown:
+
+Center of Pressure: X=-0.035458Z+34.579208 m.
+
+NOTE: Multiply forces by the non-dimensional factor: 2985038.585495, and the reference factor: 1.000000
+to obtain the dimensional force.
+
+Total CL:       0.857705 | Pressure (  100%):    0.858800 | Friction (    0%):   -0.001096 | Momentum (    0%):    0.000000
+Total CD:       0.245445 | Pressure (   98%):    0.241534 | Friction (    1%):    0.003911 | Momentum (    0%):    0.000000
+Total CSF:     -0.000132 | Pressure (   88%):   -0.000117 | Friction (   11%):   -0.000015 | Momentum (    0%):    0.000000
+Total CL/CD:    3.494488 | Pressure (  101%):    3.555605 | Friction (   -8%):   -0.280119 | Momentum (    0%):    0.000000
+Total CMx:     -0.001299 | Pressure (  100%):   -0.001300 | Friction (    0%):    0.000001 | Momentum (    0%):    0.000000
+Total CMy:     -1.198915 | Pressure (   99%):   -1.198873 | Friction (    0%):   -0.000042 | Momentum (    0%):    0.000000
+Total CMz:     -0.000193 | Pressure (   91%):   -0.000177 | Friction (    8%):   -0.000016 | Momentum (    0%):    0.000000
+Total CFx:     -0.031613 | Pressure (  112%):   -0.035671 | Friction (  -12%):    0.004058 | Momentum (    0%):    0.000000
+Total CFy:     -0.000132 | Pressure (   88%):   -0.000117 | Friction (   11%):   -0.000015 | Momentum (    0%):    0.000000
+Total CFz:      0.891573 | Pressure (   99%):    0.891406 | Friction (    0%):    0.000167 | Momentum (    0%):    0.000000
+
+
+Surface name: wall
+
+Total CL    (   99%):    0.857705 | Pressure (  100%):    0.858800 | Friction (    0%):   -0.001096 | Momentum (    0%):    0.000000
+Total CD    (   99%):    0.245445 | Pressure (   98%):    0.241534 | Friction (    1%):    0.003911 | Momentum (    0%):    0.000000
+Total CSF   (  100%):   -0.000132 | Pressure (   88%):   -0.000117 | Friction (   11%):   -0.000015 | Momentum (    0%):    0.000000
+Total CL/CD (   99%):    3.494488 | Pressure (  101%):    3.555605 | Friction (   -8%):   -0.280119 | Momentum (    0%):    0.000000
+Total CMx   (  100%):   -0.001299 | Pressure (  100%):   -0.001300 | Friction (    0%):    0.000001 | Momentum (    0%):    0.000000
+Total CMy   (  100%):   -1.198915 | Pressure (   99%):   -1.198873 | Friction (    0%):   -0.000042 | Momentum (    0%):    0.000000
+Total CMz   (  100%):   -0.000193 | Pressure (   91%):   -0.000177 | Friction (    8%):   -0.000016 | Momentum (    0%):    0.000000
+Total CFx   (  100%):   -0.031613 | Pressure (  112%):   -0.035671 | Friction (  -12%):    0.004058 | Momentum (    0%):    0.000000
+Total CFy   (  100%):   -0.000132 | Pressure (   88%):   -0.000117 | Friction (   11%):   -0.000015 | Momentum (    0%):    0.000000
+Total CFz   (   99%):    0.891573 | Pressure (   99%):    0.891406 | Friction (    0%):    0.000167 | Momentum (    0%):    0.000000
+

example/18.0degAOA/surface_and_volume_flow.zip

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example/19.0degAOA/surface_and_volume_flow.zip

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