Heat-transfer measurements boundary-layer transition, and the effects of superpolishing observed in two free-flight tests up to Mach number 5.0 at Reynolds number per foot up to 8 x 106

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dc.contributor.authorHall, James Rudyarden
dc.contributor.departmentAerospace Engineeringen
dc.date.accessioned2015-06-26T20:54:53Zen
dc.date.available2015-06-26T20:54:53Zen
dc.date.issued1961en
dc.description.degreeMaster of Scienceen
dc.format.extent93 leavesen
dc.format.mimetypeapplication/pdfen
dc.identifier.urihttp://hdl.handle.net/10919/53805en
dc.language.isoen_USen
dc.publisherVirginia Polytechnic Instituteen
dc.relation.isformatofOCLC# 20188818en
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V855 1961.H34en
dc.subject.lcshHeat -- Transmissionen
dc.subject.lcshBoundary layeren
dc.subject.lcshAirplanes -- Flight testingen
dc.titleHeat-transfer measurements boundary-layer transition, and the effects of superpolishing observed in two free-flight tests up to Mach number 5.0 at Reynolds number per foot up to 8 x 106en
dc.typeThesisen
dc.type.dcmitypeTexten
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorVirginia Polytechnic Instituteen
thesis.degree.levelmastersen
thesis.degree.nameMaster of Scienceen

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