Flamelet Combustion Modeling and Detached Eddy Simulation of a Rocket Model Combustor with Capacitive Heating
Master Thesis
(2018)
Author(s)
W.F. Holtslag (TU Delft - Aerospace Engineering)
Faculty
Aerospace Engineering
Copyright
© 2018 Wouter Holtslag
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https://resolver.tudelft.nl/uuid:71ce46ec-e667-4ce1-89be-a474de89f847
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Publication Year
2018
Language
English
Copyright
© 2018 Wouter Holtslag
Graduation Date
02-02-2018
Awarding Institution
Delft University of Technology
Programme
['Aerospace Engineering']
Faculty
Aerospace Engineering
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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.