Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation
The present work was conducted with the intent of developing a high-fidelity numerical model of a unique combustion flow problem combining multi-phase fuel injection with substantial momentum and temperature into a highly complex turbulent flow. This important problem is very different from typical...
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| Format: | Others |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/28928 http://scholar.lib.vt.edu/theses/available/etd-09102008-134309/ |