An investigation of compressible flows with large whirl components
Approved for public release, distribution is unlimited. === This investigation was conducted to determine the losses in the scroll and inlet guide vanes of a dual discharge, radial-inflow turbine. Difficulties are encountered in such tests because the air is discharged from the guide vanes with a la...
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| Language: | en_US |
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Monterey, California. U.S. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/12403 |