Effects of surface heating on the laminar boundary layer of a two-dimensional, Mach three wind tunnel nozzle

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dc.contributor.authorBrogan, Torence P.en
dc.date.accessioned2015-05-12T20:30:27Z
dc.date.available2015-05-12T20:30:27Z
dc.date.issued1995en
dc.identifier.urihttps://scholarworks.montana.edu/handle/1/7554en
dc.language.isoenen
dc.publisherMontana State University - Bozeman, College of Engineeringen
dc.rights.holderCopyright 1995 by Torence P. Broganen
dc.subject.lcshSupersonic wind tunnelsen
dc.subject.lcshBoundary layeren
dc.titleEffects of surface heating on the laminar boundary layer of a two-dimensional, Mach three wind tunnel nozzleen
dc.typeThesisen
thesis.catalog.ckey319017en
thesis.degree.departmentMechanical & Industrial Engineering.en
thesis.degree.genreThesisen
thesis.degree.nameMSen
thesis.format.extentfirstpage1en
thesis.format.extentlastpage181en

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