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A Method to Compute Flameout Limits of Scramjet-Powered Hypersonic Vehicles

dc.contributor.authorMbagwu, Chukwuka
dc.contributor.authorDriscoll, James F.
dc.date.accessioned2018-01-03T17:15:35Z
dc.date.available2018-01-03T17:15:35Z
dc.date.issued2015-07-23
dc.identifier.citationMbagwu, Chukwuka; Driscoll, James F. (2015). "A Method to Compute Flameout Limits of Scramjet-Powered Hypersonic Vehicles." 51st AIAA/SAE/ASEE Joint Propulsion Conference
dc.identifier.urihttps://hdl.handle.net/2027.42/140540
dc.publisherAmerican Institute of Aeronautics and Astronautics
dc.relation.ispartofseriesAIAA Propulsion and Energy Forum
dc.titleA Method to Compute Flameout Limits of Scramjet-Powered Hypersonic Vehicles
dc.typeConference Paperen_US
dc.subject.hlbsecondlevelAerospace Engineering
dc.subject.hlbtoplevelEngineering
dc.description.peerreviewedPeer Reviewed
dc.description.bitstreamurlhttps://deepblue.lib.umich.edu/bitstream/2027.42/140540/1/6.2015-3749.pdf
dc.identifier.doi10.2514/6.2015-3749
dc.identifier.source51st AIAA/SAE/ASEE Joint Propulsion Conference
dc.owningcollnameAerospace Engineering, Department of


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