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dc.contributor.authorKing, Peter Samuelen_US
dc.date.accessioned2015-07-10T18:51:00Z
dc.date.available2015-07-10T18:51:00Z
dc.date.issued1989en_US
dc.identifier.urihttp://hdl.handle.net/10919/54377
dc.format.extentxii, 162 leavesen_US
dc.format.mimetypeapplication/pdfen_US
dc.language.isoen_USen_US
dc.publisherVirginia Polytechnic Institute and State Universityen_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 1989.K435en_US
dc.subject.lcshAerodynamics, Supersonicen_US
dc.subject.lcshAir flowen_US
dc.titleCombined tangential-normal injection into a supersonic flowen_US
dc.typeThesisen_US
dc.contributor.departmentAerospace Engineeringen_US
dc.description.degreeMaster of Scienceen_US
dc.identifier.oclc19836662en_US
thesis.degree.nameMaster of Scienceen_US
thesis.degree.levelmastersen_US
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen_US
thesis.degree.disciplineAerospace Engineeringen_US
dc.type.dcmitypeTexten_US


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