Flamelet Combustion Modeling and Detached Eddy Simulation of a Rocket Model Combustor with Capacitive Heating
Wouter Holtslag (TU Delft - Aerospace Engineering)
Stefan Hickel – Mentor
Julian Zips – Mentor
Michael Pfitzner – Mentor
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Abstract
The Steady Laminar Flamelet Combustion Model was used in combination with the Improved Delayed Detached Eddy turbulence model. A model rocket combustor was simulated with these models. Combustion was performed with gaseous methane and oxygen, injected non-premixed. Experimental data was available for the pressure and wal heat flux to validate the simulation model.