[Taimour]

I am trying to run my own case for a simple cylinder

also I attached a picture at the end for showing the physical groups of INLET OUTLET WALLS AND CYLINDER


now I am getting this error

D:\Productividad\SU2\bin\CASES\C4>SU2_Mesh D:\Productividad\SU2\bin\CASES\C4\mesh_cylinder.su 2
'SU2_Mesh' is not recognized as an internal or external command,
operable program or batch file.

D:\Productividad\SU2\bin\CASES\C4>ren poly_cylinder.txt poly_cylinder.cfg

D:\Productividad\SU2\bin\CASES\C4>SU2_CFD poly_cylinder.cfg

-------------------------------------------------------------------------
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| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
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| (http://su2foundation.org) |
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-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Incompressible Laminar Navier-Stokes' equations.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0.25, 0, 0).
Surface(s) where the force coefficients are evaluated: CYLINDER.

Surface(s) plotted in the output file: CYLINDER.
Input mesh file name: mesh_cylinder.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Flux difference splitting (FDS) upwind scheme for the flow inviscid terms.
Second order integration in space, with slope limiter.
No slope-limiting method.
Average of gradients with correction (viscous flow terms).
Gradient for upwind reconstruction: Green-Gauss.
Gradient for viscous and source terms: Green-Gauss.

--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-15.
Max number of linear iterations: 10.
No CFL adaptation.
Courant-Friedrichs-Lewy number: 1e+03

------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 2000.
Begin convergence monitoring at iteration 10.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-06.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| PARAVIEW| 250|
| SURFACE_PARAVIEW| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown.dat.
Surface file name: surface_flow.
Volume file name: flow.
Restart file name: restart_flow.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Far-field| farfield|
+-----------------------------------------------------------------------+
| Inlet boundary| INLET|
+-----------------------------------------------------------------------+
| Outlet boundary| OUTLET|
+-----------------------------------------------------------------------+
| Isothermal wall| CYLINDER|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: INNER_ITER, RMS_PRESSURE, RMS_TEMPERATURE, LIFT, DRAG, TOTAL_HEATFLUX
History output group(s): ITER, RMS_RES
Convergence field(s): RMS_PRESSURE
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
13072 grid points.
12836 volume elements.
4 surface markers.
52 boundary elements in index 0 (Marker = INLET_).


Error in "short unsigned int CConfig::GetMarker_CfgFile_TagBound(const string&) const":
-------------------------------------------------------------------------
The configuration file doesn't have any definition for marker INLET_
------------------------------ Error Exit -------------------------------



job aborted:
[ranks] message

[0] application aborted
aborting MPI_COMM_WORLD (comm=0x44000000), error 1, comm rank 0

PLEASE HELP, THANK YOU.

[bigfootedrockmidget]

There seems to be an extra underscore in the marker name.