Thrust augmentation for a small turbojet engine
Approved for public release; distribution is unlimited === A Sophia J450 (nine pounds of thrust) gas turbine engine was used first to examine the thrust augmentation generated using an ejector shroud. Experimental results obtained with and without the ejector were compared with performance predicted...
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Language: | en_US |
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Monterey, California. Naval Postgraduate School
2012
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Online Access: | http://hdl.handle.net/10945/9074 |