Simulations of a Sub-scale Liquid Rocket Engine: Transient Heat Transfer in a Real Gas Environment
The prediction of transient phenomena inside Liquid Rocket Engines (LREs) has not been feasible until now because of the many challenges posed by the operating conditions inside the combustion chamber. Especially, the departure from ideal gas because of the cryogenic injection in a high-pressure...
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| Format: | Others |
| Language: | en_US |
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Georgia Institute of Technology
2007
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| Online Access: | http://hdl.handle.net/1853/14140 |