Large-eddy simulations of high-pressure shear coaxial flows relevant for H2/O2 rocket engines
The understanding and prediction of transient phenomena inside Liquid Rocket Engines (LREs) have been very difficult because of the many challenges posed by the conditions inside the combustion chamber. This is especially true for injectors involving liquid oxygen LOX and gaseous hydrogen GH₂. A wid...
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Georgia Institute of Technology
2013
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| Online Access: | http://hdl.handle.net/1853/47522 |