Thermal gas radiation modelling for CFD simulation of rocket thrust chamber
Methane and oxygen are a promising propellant combination in future rocket propulsion engines mainly due to its advantages like reusability and cost reduction. In order to have a comprehensive understanding of this propellant combination extensive research work is being done. Especially, for reusabl...
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| Format: | Others |
| Language: | English |
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KTH, Kraft- och värmeteknologi
2019
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-261230 |