Numerical study with computational fluid dynamics of hybrid rocket engine.
In this thesis a Large Eddy Simulation (LES) of a hybrid rocket engine burning ethylene (C2H4) in nitrous oxide (N2O) is explored. This is done primarily using a solver and solution scheme provided by the Swedish Defence Research Agency (FOI) and an (at this date) unpublished chemistry model. This s...
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| Format: | Others |
| Language: | English |
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Luleå tekniska universitet, Rymdteknik
2020
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-82037 |