gaetan3
Aerospace
- Mar 24, 2005
- 2
I need to do some thermal analysis in a combustion chamber, image it just like a tube.I have a temperature profile that I can assume constant along different tracts of the cylinder. My problem is that Pro E merges all the surface of the cylinder therefore I cannot assign different boundary conditions on the different parts of the surface. How can I keep separate different parts, or how can I separate them for my thermal analysis.Please help me