Reduced-Order Modeling of Hypersonic Unsteady Aerodynamics Due to Multi-Modal Oscillations

Skujins, Torstens; Cesnik, Carlos E. S.

Reduced-Order Modeling of Hypersonic Unsteady Aerodynamics Due to Multi-Modal Oscillations

dc.contributor.author	Skujins, Torstens	en_US
dc.contributor.author	Cesnik, Carlos E. S.	en_US
dc.date.accessioned	2012-04-05T20:36:31Z
dc.date.available	2012-04-05T20:36:31Z
dc.date.issued	2011	en_US
dc.identifier.citation	Skujins, Torstens; Cesnik, Carlos (2011). "Reduced-Order Modeling of Hypersonic Unsteady Aerodynamics Due to Multi-Modal Oscillations." 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference , San Francisco, California, Apr. 11-14, 2011, AIAA-2011-2341. <http://hdl.handle.net/2027.42/90672>	en_US
dc.identifier.other	AIAA-2011-2341	en_US
dc.identifier.uri	https://hdl.handle.net/2027.42/90672
dc.publisher	American Institute of Aeronautics and Astronautics	en_US
dc.title	Reduced-Order Modeling of Hypersonic Unsteady Aerodynamics Due to Multi-Modal Oscillations	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	en_US
dc.identifier.pmid	6060360	en_US
dc.description.bitstreamurl	http://deepblue.lib.umich.edu/bitstream/2027.42/90672/1/AIAA-2011-2341-210.pdf
dc.owningcollname	Aerospace Engineering, Department of

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