Comparative Study of Pitch-Plunge Airfoil Aerodynamics at Transitional Reynolds Number

Lian, Yongsheng; Ol, Michael; Shyy, Wei

Comparative Study of Pitch-Plunge Airfoil Aerodynamics at Transitional Reynolds Number

dc.contributor.author	Lian, Yongsheng	en_US
dc.contributor.author	Ol, Michael	en_US
dc.contributor.author	Shyy, Wei	en_US
dc.date.accessioned	2010-06-11T17:56:25Z
dc.date.available	2010-06-11T17:56:25Z
dc.date.issued	2008	en_US
dc.identifier.citation	Lian, Yongsheng; Ol, Michael; Shyy, Wei (2008). "Comparative Study of Pitch-Plunge Airfoil Aerodynamics at Transitional Reynolds Number" AIAA-2008-652, 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 7-10, 2008. <http://hdl.handle.net/2027.42/76128>	en_US
dc.identifier.other	AIAA-2008-652	en_US
dc.identifier.uri	https://hdl.handle.net/2027.42/76128
dc.format.extent	1578461 bytes
dc.format.extent	3112 bytes
dc.format.mimetype	application/pdf
dc.format.mimetype	text/plain
dc.publisher	American Institute of Aeronautics and Astronautics	en_US
dc.title	Comparative Study of Pitch-Plunge Airfoil Aerodynamics at Transitional Reynolds Number	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.affiliationum	University of Michigan, Ann Arbor, MI	en_US
dc.contributor.affiliationum	University of Michigan, Ann Arbor, MI	en_US
dc.contributor.affiliationother	U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH	en_US
dc.description.bitstreamurl	http://deepblue.lib.umich.edu/bitstream/2027.42/76128/1/AIAA-2008-652-591.pdf
dc.owningcollname	Interdisciplinary and Peer-Reviewed

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