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Reduced-Order Aerothermoelastic Framework for Hypersonic Vehicle Control Simulation

dc.contributor.authorFalkiewicz, Nathanen_US
dc.contributor.authorCesnik, Carlos E. S.en_US
dc.contributor.authorCrowell, Andrewen_US
dc.contributor.authorMcNamara, Jacken_US
dc.date.accessioned2012-04-05T20:35:19Z
dc.date.available2012-04-05T20:35:19Z
dc.date.issued2011en_US
dc.identifier.citationFalkiewicz, Nathan; Cesnik, Carlos; Crowell, Andrew; McNamara, Jack (2011). "Reduced-Order Aerothermoelastic Framework for Hypersonic Vehicle Control Simulation." AIAA Journal, vol. 49 no. 8 (1625-1646). <http://hdl.handle.net/2027.42/90631>en_US
dc.identifier.issn0001-1452en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/90631
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleReduced-Order Aerothermoelastic Framework for Hypersonic Vehicle Control Simulationen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationotherUniversity of Michigan; University of Michigan; Ohio State University; Ohio State Universityen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/90631/1/AIAA-55319-887.pdf
dc.identifier.doi10.2514/1.55319en_US
dc.identifier.sourceAIAA Journalen_US
dc.owningcollnameAerospace Engineering, Department of


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