Simulation of combustion in a rocket engine with Ansys Fluent
>> YOUR LINK HERE: ___ http://youtube.com/watch?v=cYNq0MJmfUg
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 http://combustion.berkeley.edu/gri-me... • The chamber coordinates file is in a comment below.
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