Simulation of combustion in a rocket engine with Ansys Fluent

The rocket combustion chamber simulation project with Ansys Fluent: 10kN motor working on LOX CH4 propellants operating at sea level. Presented simulation describes combustion in a gaseous flow. Simulation of liquid-to-gas transition (phase change) should be made, including an appropriate evaporation model. Gri-Mech 3.0 combustion library is available at The chamber coordinates file is in a comment below.