Problem with rotating cylinder natural convection
Iam modelling a flow over a rotating cylinder. Iam not getting the results. The fluid domain is rectangular. Fluid is air. Density is modelled as incompressible ideal gas.
g= -9.81 Inlet at bottom of domain: pressure inlet Outlet at top of domain: pressure outlet Side walls as adiabatic walls Cylinder as wall. Grashof no= 1.56*10^6 Laminar Operating temperature =298.16 Operating density=1.184 If anything is wrong , somebody please correct me... |
What about the thermal boundary condition on the cylinder wall? And what does it mean not getting results?
|
Heat flux of 800W/m2 is given at cylinder wall.
|
All times are GMT -4. The time now is 07:45. |