|
icem hexa mesh parts pb
Hello dear colleagues,
I’m simulating a flow over a symmetrical NACA airfoil using ANSYSCFX11.so,to have a multiblock structured mesh, I have done a 2d extruded mesh using ICEM HEXA(v11).the steps followed are: 1-generating 2d geometry (airfoil+rectangular domain) using a scripts file. creating parts representing geometry families. 2-2d blocking (several operations) and 2d mesh. 3-extruding (1 layer) the 2d mesh after converting to unstructured mesh. Results: having a 2d extruded mesh. But parts still representing lines and not sides. making pb to introduce boundary conditions (inlet,outlet,wall and airfoil). please, I will be grateful to receive any idea or suggestions. |
| All times are GMT -4. The time now is 14:45. |