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Conceptual Analysis of Electron Transpiration Cooling for the Leading Edges of Hypersonic Vehicles
dc.contributor.authorAlkandry, Hicham
dc.contributor.authorHanquist, Kyle
dc.contributor.authorBoyd, Iain D.
dc.date.accessioned2018-01-03T17:13:34Z
dc.date.available2018-01-03T17:13:34Z
dc.date.issued2014-06-13
dc.identifier.citationAlkandry, Hicham; Hanquist, Kyle; Boyd, Iain D. (2014). "Conceptual Analysis of Electron Transpiration Cooling for the Leading Edges of Hypersonic Vehicles." 11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference
dc.identifier.urihttps://hdl.handle.net/2027.42/140441
dc.publisherAmerican Institute of Aeronautics and Astronautics
dc.relation.ispartofseriesAIAA AVIATION Forum
dc.titleConceptual Analysis of Electron Transpiration Cooling for the Leading Edges of 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/2027.42/140441/1/6.2014-2674.pdf
dc.identifier.doi10.2514/6.2014-2674
dc.identifier.source11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference
dc.owningcollnameAerospace Engineering, Department of


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