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Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/43531
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dc.contributor.authorSmith, Joshua Johnen
dc.contributor.authorSchneider, Gerald Manfreden
dc.contributor.authorSuslov, D.en
dc.contributor.authorOschwald, M.en
dc.contributor.authorHaidn, O.en
dc.date.issued2007en
dc.identifier.citationAerospace Science and Technology, 2007; 11 (1):39-47en
dc.identifier.issn1270-9638en
dc.identifier.urihttp://hdl.handle.net/2440/43531-
dc.descriptionCopyright © 2006 Elsevier Masson SAS All rights reserved.en
dc.description.statementofresponsibilityJoshua J. Smith, Gerald Schneider, Dmitry Suslov, Michael Oschwald and Oskar Haidnen
dc.description.urihttp://www.elsevier.com/wps/find/journaldescription.cws_home/600735/description#descriptionen
dc.language.isoenen
dc.publisherEditions Scientifiques Medicales Elsevieren
dc.relation.ispartofPropellant combustion phenomena / Luigi T. DeLuca, Paul Kuentzmann and Alexander S. Rudakov (eds.)en
dc.titleSteady-state high pressure LOx/H2 rocket engine combustionen
dc.typeJournal articleen
dc.contributor.schoolSchool of Mechanical Engineeringen
dc.identifier.doi10.1016/j.ast.2006.08.007en
Appears in Collections:Mechanical Engineering publications

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