Flamelet Combustion Modeling and Detached Eddy Simulation of a Rocket Model Combustor with Capacitive Heating

Master thesis (2018)

Authors

W.F. Holtslag Aerospace Engineering

Contributors

S. Hickel (mentor)
Julian Zips (mentor)
Faculty
Aerospace Engineering, Aerospace Engineering
Copyright: © 2018 Wouter Holtslag
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Published Date

02-02-2018

Language

English

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Faculty

Aerospace Engineering

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.

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