The design of a 3.4 by 3.4 inch supersonic wind tunnel capable of continuous operation in the range of Mach numbers between 1.50 and 3.59

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dc.contributor.authorAnderson, Euell Clayen
dc.contributor.departmentAerospace Engineeringen
dc.date.accessioned2016-05-23T14:56:51Zen
dc.date.available2016-05-23T14:56:51Zen
dc.date.issued1962en
dc.description.degreeMaster of Scienceen
dc.format.extent73 leavesen
dc.format.mimetypeapplication/pdfen
dc.identifier.urihttp://hdl.handle.net/10919/70993en
dc.language.isoen_USen
dc.publisherVirginia Polytechnic Instituteen
dc.relation.isformatofOCLC# 22579236en
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V855 1962.A549en
dc.subject.lcshSupersonic wind tunnels -- Designen
dc.subject.lcshWind tunnels -- Designen
dc.titleThe design of a 3.4 by 3.4 inch supersonic wind tunnel capable of continuous operation in the range of Mach numbers between 1.50 and 3.59en
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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