Investigation of performance improvements including application of inlet guide vanes to a cross-flow fan
Approved for public release, distribution unlimited === The inherent characteristics of a cross-flow fan allowing for easy thrust vectoring as well as potential airfoil boundary layer control make it an attractive propulsive means for a theoretical vertical takeoff and landing aircraft. However, to...
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Monterey, California. Naval Postgraduate School
2012
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Online Access: | http://hdl.handle.net/10945/4531 |