CA
C. Akkermans
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Ignition modeling in methane-oxygen rocket engines
Design and modeling of a methane-oxygen rocket engine igniter using reacting flows with computational fluid dynamics
The influence of using different chemistry model and different chemical kinetics schemes on modeling combustion inside a rocket engine igniter are investigated. An igniter for a LOX/CH4 rocket engine is designed and a CFD model is developed which is used to model the designed igniter. Verification and validation methods are discussed.
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The influence of using different chemistry model and different chemical kinetics schemes on modeling combustion inside a rocket engine igniter are investigated. An igniter for a LOX/CH4 rocket engine is designed and a CFD model is developed which is used to model the designed igniter. Verification and validation methods are discussed.
Bachelor thesis
(2014)
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C. Akkermans, F.D. Andriessen, S. Butter, R.J. Crone, G. Galatis, R.J. Grandia, B.F. Lagaune, M.R. van Reijen, N.M. van Schoote, B. Walgaard, A. Bhat, T.P. Scholcz