Experimental Investigation of Corner Flows in Rectangular Supersonic Inlets with 3D Shock-Boundary Layer Effects

Eagle, W. Ethan; Driscoll, James F.; Benek, Jack

Experimental Investigation of Corner Flows in Rectangular Supersonic Inlets with 3D Shock-Boundary Layer Effects

dc.contributor.author	Eagle, W. Ethan	en_US
dc.contributor.author	Driscoll, James F.	en_US
dc.contributor.author	Benek, Jack	en_US
dc.date.accessioned	2012-04-05T20:34:53Z
dc.date.available	2012-04-05T20:34:53Z
dc.date.issued	2011	en_US
dc.identifier.citation	Eagle, Walter; Driscoll, James; Benek, Jack (2011). "Experimental Investigation of Corner Flows in Rectangular Supersonic Inlets with 3D Shock-Boundary Layer Effects." 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, Jan. 4-7, 2011, AIAA-2011-857. <http://hdl.handle.net/2027.42/90617>	en_US
dc.identifier.other	AIAA-2011-857	en_US
dc.identifier.uri	https://hdl.handle.net/2027.42/90617
dc.publisher	American Institute of Aeronautics and Astronautics	en_US
dc.title	Experimental Investigation of Corner Flows in Rectangular Supersonic Inlets with 3D Shock-Boundary Layer Effects	en_US
dc.type	Article	en_US
dc.subject.hlbsecondlevel	Aerospace Engineering	en_US
dc.subject.hlbtoplevel	Engineering	en_US
dc.description.peerreviewed	Peer Reviewed	en_US
dc.contributor.affiliationother	University of Michigan, Ann Arbor, MI; University of Michigan, Ann Arbor, MI; Air Force Research Laboratory, Wright-Patterson AFB, OH	en_US
dc.description.bitstreamurl	http://deepblue.lib.umich.edu/bitstream/2027.42/90617/1/AIAA-2011-857-617.pdf
dc.owningcollname	Aerospace Engineering, Department of

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