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Flight Envelope Calculation of a Hypersonic Vehicle Using a First Principles-Derived Model

dc.contributor.authorDalle, Dereken_US
dc.contributor.authorTorrez, Seanen_US
dc.contributor.authorDriscoll, James F.en_US
dc.contributor.authorBolender, Michaelen_US
dc.date.accessioned2012-04-05T20:36:32Z
dc.date.available2012-04-05T20:36:32Z
dc.date.issued2011en_US
dc.identifier.citationDalle, Derek; Torrez, Sean; Driscoll, James; Bolender, Michael (2011). "Flight Envelope Calculation of a Hypersonic Vehicle Using a First Principles-Derived Model." 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference , San Francisco, California, Apr. 11-14, 2011, AIAA-2011-2368. <http://hdl.handle.net/2027.42/90673>en_US
dc.identifier.otherAIAA-2011-2368en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/90673
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleFlight Envelope Calculation of a Hypersonic Vehicle Using a First Principles-Derived Modelen_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 Arbor; USAF Research Laboratory, Wright-Patterson AFB, OHen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/90673/1/AIAA-2011-2368-297.pdf
dc.owningcollnameAerospace Engineering, Department of


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