Investigation of liquid fuel jet injection into a simulated subsonic "dump" combustor
Basic experimental studies of the injection of liquid fuel into a two dimensional flowfield designed to represent a sudden-expansion "dump" combustor were performed under cold-flow conditions. Test conditions were as follows: 0.6 entrance Mach number, 25 PSIA total pressure, and nominally...
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| Format: | Others |
| Language: | en |
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Virginia Polytechnic Institute and State University
2020
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| Online Access: | http://hdl.handle.net/10919/101411 |