[Shashank mv]

Hi, I was running a SU2 code for a 2d scramjet intake, but i am getting an error as the MARKER INLET not defined, but i have defined it in my configuration file. So can anybody tell what is the mistake i am doing. Below are the mesh and the CGNS files.
Microsoft Windows [Version 10.0.22631.5699]
(c) Microsoft Corporation. All rights reserved.

D:\SU2_8.2\bin>SU2_CFD flatplatef.cfg

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-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Laminar Navier-Stokes' equations.
Mach number: 5.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
Reynolds number: 1.30123e+06. Reference length 0.3048.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 0.3048 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Input mesh file name: Scramjetf.cgns

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
No slope-limiting method.
Average of gradients with correction (viscous flow terms).
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- 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 LU-SGS preconditioning.
Convergence criteria of the linear solver: 0.05.
Max number of linear iterations: 3.
V Multigrid Cycle, with 3 multigrid levels.
Damping factor for the residual restriction: 0.8.
Damping factor for the correction prolongation: 0.8.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 1| 0|
| 2| 3| 1| 0|
| 3| 0| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 1e+03

------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5000.
Begin convergence monitoring at iteration 10.
Residual minimum value: 1e-12.
Cauchy series min. value: 1e-10.
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.
Volume file name: vol_solution.
Restart file name: restart_flow.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| wall1|
| | wall2|
+-----------------------------------------------------------------------+
| Far-field| farfield|
| | inlet|
+-----------------------------------------------------------------------+
| Outlet boundary| Outlet1|
| | Outlet02|
+-----------------------------------------------------------------------+

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

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

Info: Ignoring the following screen output fields:
TOTAL_HEATFLUX_ON_SURFACE
Screen output fields: INNER_ITER, RMS_DENSITY, RMS_ENERGY, DRAG, SURFACE_MASSFLOW, TOTAL_HEATFLUX
History output group(s): ITER, RMS_RES
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Reading the CGNS file: Scramjetf.cgns.
WARNING: The CGNS file version (3.31) is old and may cause high memory usage issues, consider updating the file with the cgnsupdate tool.
CGNS file contains 1 database(s).
Database 1, BASE#1: cell dimension of 2, physical dimension of 3.
1 total zone(s).
Zone 1, Scramjetf: 29454 total vertices, 28958 total elements.
Loading CoordinateX values.
Loading CoordinateY values.
Number of connectivity sections is 8.
Section SURFACE_BODY_1_1 contains 28958 elements of type Quadrilateral.
Section INLET contains 106 elements of type Line.
Section WALL1 contains 389 elements of type Line.
Section WALL2 contains 132 elements of type Line.
Section OUTLET01 contains 93 elements of type Line.
Section OUTLET02 contains 13 elements of type Line.
Section FARFIELD contains 257 elements of type Line.
Section SURFACE_BODY_1_1_1D contains 191 elements of type Line.
Loading volume section SURFACE_BODY_1_1 from file.
Loading surface section INLET from file.
Loading surface section WALL1 from file.
Loading surface section WALL2 from file.
Loading surface section OUTLET01 from file.
Loading surface section OUTLET02 from file.
Loading surface section FARFIELD from file.
Loading surface section SURFACE_BODY_1_1_1D from file.
Two dimensional problem.
29454 grid points.
28958 volume elements.
7 surface markers.
106 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 -------------------------------

[bigfootedrockmidget]

In your .cfg file, what does your entry for MARKER_INLET or MARKER_INLET_SUPERSONIC look like?