Unsteady separation point injection for pressure recovery improvement in high subsonic diffusers
Serpentine inlet ducts on modem tactical aircraft distort the inlet flow and decrease pressure recovery at the aerodynamic interface plane (AIP). Current inlet designs are more aggressive, increasing distortion and decreasing pressure recovery at the AIP. Often the flow separates from the wall of th...
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2012
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| Online Access: | http://hdl.handle.net/10945/11024 |