Show simple item record

dc.contributor.authorAnderson, Euell Clayen_US
dc.date.accessioned2016-05-23T14:56:51Z
dc.date.available2016-05-23T14:56:51Z
dc.date.issued1962en_US
dc.identifier.urihttp://hdl.handle.net/10919/70993
dc.format.extent73 leavesen_US
dc.format.mimetypeapplication/pdfen_US
dc.language.isoen_USen_US
dc.publisherVirginia Polytechnic Instituteen_US
dc.rightsThis Item is protected by copyright and/or related rights. Some uses of this Item may be deemed fair and permitted by law even without permission from the rights holder(s), or the rights holder(s) may have licensed the work for use under certain conditions. For other uses you need to obtain permission from the rights holder(s).en_US
dc.subject.lccLD5655.V855 1962.A549en_US
dc.subject.lcshSupersonic wind tunnels -- Designen_US
dc.subject.lcshWind tunnels -- Designen_US
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_US
dc.typeThesisen_US
dc.contributor.departmentAerospace Engineeringen_US
dc.description.degreeMaster of Scienceen_US
dc.identifier.oclc22579236en_US
thesis.degree.nameMaster of Scienceen_US
thesis.degree.levelmastersen_US
thesis.degree.grantorVirginia Polytechnic Instituteen_US
thesis.degree.disciplineAerospace Engineeringen_US
dc.type.dcmitypeTexten_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record