-
Notifications
You must be signed in to change notification settings - Fork 843
Commit
This commit does not belong to any branch on this repository, and may belong to a fork outside of the repository.
Merge pull request #2278 from BerkeCan97/fix_marker_engine_inflow
Fix marker engine inflow
- Loading branch information
Showing
5 changed files
with
236 additions
and
1 deletion.
There are no files selected for viewing
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
222 changes: 222 additions & 0 deletions
222
TestCases/engine/marker_engine_inflow/inv_channel_engine_inflow.cfg
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
| Original file line number | Diff line number | Diff line change |
|---|---|---|
| @@ -0,0 +1,222 @@ | ||
| %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% | ||
| % % | ||
| % SU2 configuration file % | ||
| % Case description: Inviscid, internal flow over a bump in a channel with % | ||
| % prescribed Mach number for outlet BC % | ||
| % Author: Thomas D. Economon , Berke C. Deveci % | ||
| % Institution: Stanford University % | ||
| % Date: 2024.05.28 % | ||
| % File Version 8.0.1 "Harrier" % | ||
| % % | ||
| %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% | ||
|
|
||
| % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------% | ||
| % | ||
| % Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA) | ||
| % | ||
| SOLVER= EULER | ||
| % | ||
| % Mathematical problem (DIRECT, CONTINUOUS_ADJOINT) | ||
| MATH_PROBLEM= DIRECT | ||
| % | ||
| % Restart solution (NO, YES) | ||
| RESTART_SOL= NO | ||
|
|
||
| % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------% | ||
| % | ||
| % Mach number (non-dimensional, based on the free-stream values) | ||
| MACH_NUMBER= 0.1 | ||
| % | ||
| % Angle of attack (degrees, only for compressible flows) | ||
| AOA= 0.0 | ||
| % | ||
| % Side-slip angle (degrees, only for compressible flows) | ||
| SIDESLIP_ANGLE= 0.0 | ||
| % | ||
| % Free-stream pressure (101325.0 N/m^2 by default) | ||
| FREESTREAM_PRESSURE= 101300.0 | ||
| % | ||
| % Free-stream temperature (288.15 K by default) | ||
| FREESTREAM_TEMPERATURE= 288.0 | ||
|
|
||
| % ---------------------- 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 | ||
|
|
||
| % -------------------- BOUNDARY CONDITION DEFINITION --------------------------% | ||
| % | ||
| % Euler wall boundary marker(s) (NONE = no marker) | ||
| MARKER_EULER= ( upper_wall, lower_wall ) | ||
| % | ||
| % Inlet boundary type (TOTAL_CONDITIONS, MASS_FLOW) | ||
| INLET_TYPE= TOTAL_CONDITIONS | ||
| % | ||
| % Inlet boundary marker(s) (NONE = no marker) | ||
| % Format: ( inlet marker, total temperature, total pressure, flow_direction_x, | ||
| % flow_direction_y, flow_direction_z, ... ) where flow_direction is | ||
| % a unit vector. | ||
| % Default: Mach ~ 0.1 | ||
| MARKER_INLET= ( inlet, 288.6, 102010.0, 1.0, 0.0, 0.0 ) | ||
| % Comment above line and uncomment next for Mach ~ 0.7 (transonic) | ||
| %MARKER_INLET= ( inlet, 316.224, 140513.23, 1.0, 0.0, 0.0 ) | ||
| % | ||
| % Engine inflow boundary marker(s) (NONE = no marker) | ||
| % Format: (engine inflow marker, fan face Mach, ... ) | ||
| MARKER_ENGINE_INFLOW= ( outlet, 0.1) | ||
| ENGINE_INFLOW_TYPE= FAN_FACE_MACH | ||
| % Damping factor for the engine inflow. | ||
| DAMP_ENGINE_INFLOW= 0.2 | ||
| % Evaluation frequency for engine marker values | ||
| BC_EVAL_FREQ = 1 | ||
|
|
||
| % ------------------------ SURFACES IDENTIFICATION ----------------------------% | ||
| % | ||
| % Marker(s) of the surface to be plotted or designed | ||
| MARKER_PLOTTING= ( lower_wall ) | ||
| % | ||
| % Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated | ||
| MARKER_MONITORING= ( upper_wall, lower_wall ) | ||
|
|
||
| % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------% | ||
| % | ||
| % Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES) | ||
| NUM_METHOD_GRAD= GREEN_GAUSS | ||
| % | ||
| % Courant-Friedrichs-Lewy condition of the finest grid | ||
| CFL_NUMBER= 50.0 | ||
| % | ||
| % Adaptive CFL number (NO, YES) | ||
| CFL_ADAPT= YES | ||
| % | ||
| % Parameters of the adaptive CFL number (factor down, factor up, CFL min value, | ||
| % CFL max value ) | ||
| CFL_ADAPT_PARAM= ( 0.1, 2.0, 50.0, 1e10 ) | ||
| % | ||
| % Runge-Kutta alpha coefficients | ||
| RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 ) | ||
| % | ||
| % Number of total iterations | ||
| ITER= 999999 | ||
|
|
||
| % ------------------------ LINEAR SOLVER DEFINITION ---------------------------% | ||
| % | ||
| % Linear solver for implicit formulations (BCGSTAB, FGMRES) | ||
| LINEAR_SOLVER= FGMRES | ||
| % | ||
| % Preconditioner of the Krylov linear solver (ILU, JACOBI, LINELET, LU_SGS) | ||
| LINEAR_SOLVER_PREC= ILU | ||
| % | ||
| % Minimum error of the linear solver for implicit formulations | ||
| LINEAR_SOLVER_ERROR= 1E-10 | ||
| % | ||
| % Max number of iterations of the linear solver for the implicit formulation | ||
| LINEAR_SOLVER_ITER= 20 | ||
|
|
||
| % -------------------------- MULTIGRID PARAMETERS -----------------------------% | ||
| % | ||
| % Multi-Grid Levels (0 = no multi-grid) | ||
| MGLEVEL= 3 | ||
| % | ||
| % Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE) | ||
| MGCYCLE= W_CYCLE | ||
| % | ||
| % Multi-grid pre-smoothing level | ||
| MG_PRE_SMOOTH= ( 1, 2, 3, 3 ) | ||
| % | ||
| % 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= 1.0 | ||
| % | ||
| % Damping factor for the correction prolongation | ||
| MG_DAMP_PROLONGATION= 1.0 | ||
|
|
||
| % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------% | ||
| % | ||
| % Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC, | ||
| % TURKEL_PREC, MSW) | ||
| CONV_NUM_METHOD_FLOW= JST | ||
| % | ||
| % 2nd and 4th order artificial dissipation coefficients | ||
| JST_SENSOR_COEFF= ( 0.5, 0.02 ) | ||
| % | ||
| % Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT) | ||
| TIME_DISCRE_FLOW= EULER_IMPLICIT | ||
|
|
||
| % --------------------------- CONVERGENCE PARAMETERS --------------------------% | ||
| % | ||
| % Convergence criteria (CAUCHY, RESIDUAL) | ||
| CONV_FIELD= RMS_DENSITY | ||
| % | ||
| % Min value of the residual (log10 of the residual) | ||
| CONV_RESIDUAL_MINVAL= -10 | ||
| % | ||
| % Start convergence criteria at iteration number | ||
| CONV_STARTITER= 10 | ||
| % | ||
| % Number of elements to apply the criteria | ||
| CONV_CAUCHY_ELEMS= 100 | ||
| % | ||
| % Epsilon to control the series convergence | ||
| CONV_CAUCHY_EPS= 1E-10 | ||
|
|
||
| % ------------------------- INPUT/OUTPUT INFORMATION --------------------------% | ||
| % | ||
| % Mesh input file | ||
| MESH_FILENAME= ../../euler/channel/mesh_channel_256x128.su2 | ||
| % | ||
| % Mesh input file format (SU2, CGNS, NETCDF_ASCII) | ||
| MESH_FORMAT= SU2 | ||
| % | ||
| % Mesh output file | ||
| MESH_OUT_FILENAME= mesh_out.su2 | ||
| % | ||
| % Restart flow input file | ||
| SOLUTION_FILENAME= solution_flow.dat | ||
| % | ||
| % Restart adjoint input file | ||
| SOLUTION_ADJ_FILENAME= solution_adj.dat | ||
| % | ||
| % Output file format (PARAVIEW, TECPLOT, STL) | ||
| TABULAR_FORMAT= CSV | ||
| % | ||
| % Output file convergence history (w/o extension) | ||
| CONV_FILENAME= history | ||
| % | ||
| % Output file restart flow | ||
| RESTART_FILENAME= restart_flow.dat | ||
| % | ||
| % Output file restart adjoint | ||
| RESTART_ADJ_FILENAME= restart_adj.dat | ||
| % | ||
| % Output file flow (w/o extension) variables | ||
| VOLUME_FILENAME= flow | ||
| % | ||
| % Output file adjoint (w/o extension) variables | ||
| VOLUME_ADJ_FILENAME= adjoint | ||
| % | ||
| % Output objective function gradient (using continuous adjoint) | ||
| GRAD_OBJFUNC_FILENAME= of_grad.dat | ||
| % | ||
| % Output file surface flow coefficient (w/o extension) | ||
| SURFACE_FILENAME= surface_flow | ||
| % | ||
| % Output file surface adjoint coefficient (w/o extension) | ||
| SURFACE_ADJ_FILENAME= surface_adjoint | ||
| % | ||
| % | ||
| % Screen output | ||
| SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_ENERGY, LIFT, DRAG) |
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters