[leo_NM]

Good afternoon.

I'm dealing with ICEM steep learning curve, I solved the problem (thanks guys from CFDonline) with the points of the airfoil. Now I'm having problens with Fluent recognizing my boundary conditions.

The method I used was:

1- Draw the farfield and defined the curves with names ENTRADA (inlet); SAIDA(outlet), PAREDES(upper and down wall) and AEROFOLIO (airfoil).

2- I saved *.msh using ANSYS Fluent and NASTRAN as solver. I Know that the ideal case would be ANSYS Fluent and ANSYS as solver, but this is the third time I try to define the boundary, in the other tries I selected ANSYS Fluent and ANSYS as solver.

3- Defined the boundary conditions ( see the pictures).

How can I configure ICEM + Fluent to recognize my Inlet B.C.

I attached some images.

thanks !

[Far]

you need separate curve and edge for ICEM to recognise the boundary condition.

http://www.cfd-online.com/Forums/ans...em-fluent.html