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Preliminary Design Methodology for Hypersonic Engine Flowpaths

dc.contributor.authorTorrez, Seanen_US
dc.contributor.authorDriscoll, James F.en_US
dc.contributor.authorDalle, Dereken_US
dc.contributor.authorFotia, Matthewen_US
dc.date.accessioned2010-06-11T18:37:34Z
dc.date.available2010-06-11T18:37:34Z
dc.date.issued2009en_US
dc.identifier.citationTorrez, Sean; Driscoll, James; Dalle, Derek; Fotia, Matthew (2009). "Preliminary Design Methodology for Hypersonic Engine Flowpaths" AIAA-2009-7289, 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, Oct. 19-22, 2009. <http://hdl.handle.net/2027.42/76758>en_US
dc.identifier.otherAIAA-2009-7289en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/76758
dc.format.extent1498930 bytes
dc.format.extent3112 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titlePreliminary Design Methodology for Hypersonic Engine Flowpathsen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumUniversity of Michigan, Ann Arbor, MIen_US
dc.contributor.affiliationumUniversity of Michigan, Ann Arbor, MIen_US
dc.contributor.affiliationumUniversity of Michigan, Ann Arbor, MIen_US
dc.contributor.affiliationumUniversity of Michigan, Ann Arbor, MIen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/76758/1/AIAA-2009-7289-311.pdf
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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