Hot-wire surveys in the vortex wake downstream of a three-percent fighter aircraft model at high angles of attack
Approved for public release; distribution is unlimited. === A low-speed wind tunnel investigation was conducted to examine the vortex wake downstream of a three-percent scale model of the YF-17 lightweight fighter prototype at high angles of attack. The study was in support of NASA ames Research Cen...
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Monterey, California: Naval Postgraduate School
2013
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| Online Access: | http://hdl.handle.net/10945/27586 |