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Design of Dual-Mode Engine Flowpaths for Hypersonic Vehicles Using Reduced-Order Models
dc.contributor.authorTorrez, Seanen_US
dc.contributor.authorDalle, Dereken_US
dc.contributor.authorDriscoll, James F.en_US
dc.date.accessioned2012-04-05T20:36:33Z
dc.date.available2012-04-05T20:36:33Z
dc.date.issued2011en_US
dc.identifier.citationTorrez, Sean; Dalle, Derek; Driscoll, James (2011). "Design of Dual-Mode Engine Flowpaths for Hypersonic Vehicles Using Reduced-Order Models." 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference , San Francisco, California, Apr. 11-14, 2011, AIAA-2011-2380. <http://hdl.handle.net/2027.42/90674>en_US
dc.identifier.otherAIAA-2011-2380en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/90674
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleDesign of Dual-Mode Engine Flowpaths for Hypersonic Vehicles Using Reduced-Order Modelsen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationotherUniversity of Michigan, Ann Arbor; University of Michigan, Ann Arbor; University of Michigan, Ann Arboren_US
dc.identifier.pmid21913044en_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/90674/1/AIAA-2011-2380-351.pdf
dc.owningcollnameAerospace Engineering, Department of


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