Experiments on vortex energy recovery by favourable interference between wing and shrouded fan
Wind tunnel tests were conducted to investi gate t he effect of placing a propulsion fan behind the tip of a li.tting ring for the purpose of recovering the energy in the trailing vortex. Results indicated tha~ significant increase of thrust could be obtained as a result of vortex energy recovery. I...
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| Format: | Others |
| Language: | en_US |
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Wichita State University
2013
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| Online Access: | http://hdl.handle.net/10057/6641 |