[AS_Aero]

Hi All

I am trying to do an LES Simulation for internal incompressible flow and I am getting some errors although I am intializing with zero veloctiy and inlet pressure

Also I am getting some error after initializing with the velocity and pressure as my inlet pressure


My case is
Inlet BC'n : Pressure : 6 bar
Outlet BC'n : Massflow rate : 0.058kg/sec
Ref Pressure : 1 atm
Initialization done with
u,V,w = 0 m/s
Pressure (Relative ) = 6 bar


This is what I got as an error below


_______

COEFFICIENT LOOP ITERATION = 2 CPU SECONDS = 8.578E+02
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+

+--------------------------------------------------------------------+
| ERROR #004100018 has occurred in subroutine FINMES. |
| Message: |
| Fatal overflow in linear solver. |
+--------------------------------------------------------------------+

+--------------------------------------------------------------------+
| An error has occurred in cfx5solve: |
| |
| The ANSYS CFX solver could not be started, or exited with return |
| code 255. No results file has been created. |
+--------------------------------------------------------------------+

End of solution stage.

_______


This is what I got .

Thanks