TITLE : GAS-TURBINE COMBUSTION CHAMBER (LIBRARY CASE 493)

BY : CHAM Consultancy Team

DETAILS :

• In this application a section of a cylindrical combustion chamber is modelled using polar coordinates.

• Fuel and air enter the chamber at the bottom right of the section (i.e. in the centre of the cylinder). There are two further oxidant inlets at the top of the section and the gases leave the chamber on the left.

• The k-e turbulence model and the Eddy-break-up combustion models are used.

1. Boundary patches
2. Temperature contours
3. Temperature contours (view x)
4. Temperature contours (view y)
5. Temperature contours (view z)
6. Velocity vectors
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