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dc.contributor.authorBowersox, Rodney Dale Welchen_US
dc.date.accessioned2014-03-14T21:31:06Z
dc.date.available2014-03-14T21:31:06Z
dc.date.issued1990-01-07en_US
dc.identifier.otheretd-03122009-040531en_US
dc.identifier.urihttp://hdl.handle.net/10919/41454
dc.description.abstractCurrent emphasis on sustained supersonic and hypersonic cruise has sparked interest in more efficient power plants for this flight regime. Cycle studies have shown that the turbofan engine equipped with a supersonic through-flow fan, capable of accepting supersonic axial flow from the inlet, has the potential to be very efficient at the supersonic cruise condition.en_US
dc.format.mediumBTDen_US
dc.publisherVirginia Techen_US
dc.relation.haspartLD5655.V855_1990.B683.pdfen_US
dc.subjectAirplanesen_US
dc.subject.lccLD5655.V855 1990.B683en_US
dc.titleMeanflow and turbulence measurements in the wake of a supersonic through-flow cascadeen_US
dc.typeThesisen_US
dc.contributor.departmentAerospace Engineeringen_US
dc.description.degreeMaster of Scienceen_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.contributor.committeechairSchetz, Joseph A.en_US
dc.contributor.committeememberNg, Faien_US
dc.contributor.committeememberJakubowski, Antoni K.en_US
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-03122009-040531/en_US
dc.date.sdate2009-03-12en_US
dc.date.rdate2009-03-12
dc.date.adate2009-03-12en_US


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