A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact

dc.contributor.authorReid, Terry Vincenten
dc.contributor.committeechairNg, Faien
dc.contributor.committeememberScott, Elaine P.en
dc.contributor.committeememberNelson, Douglas J.en
dc.contributor.committeememberDiller, Thomas E.en
dc.contributor.committeememberSchetz, Joseph A.en
dc.contributor.departmentMechanical Engineeringen
dc.date.accessioned2014-03-14T20:06:41Zen
dc.date.adate1999-02-05en
dc.date.available2014-03-14T20:06:41Zen
dc.date.issued1998-04-30en
dc.date.rdate1999-02-05en
dc.date.sdate1999-01-10en
dc.description.abstractThe effects of shock wave impact on unsteady turbine heat transfer are investigated. A numerical approach is developed to simulate the flow physics present in a previously performed unsteady wind tunnel experiment. The windtunnel experiment included unheated and heated flows over a cascade of highly loaded turbine blades. After the flow over the blades was established, a single shock with a pressure ratio of 1.1 was introduced into the wind tunnel test section. A single blade was equipped with pressure transducers and heat flux microsensors. As the shock wave strikes the blade, time resolved pressure, temperature, and heat transfer data were recorded.en
dc.description.degreePh. D.en
dc.identifier.otheretd-011099-132537en
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-011099-132537/en
dc.identifier.urihttp://hdl.handle.net/10919/25983en
dc.publisherVirginia Techen
dc.relation.haspartChapt5.pdfen
dc.relation.haspartChapt4.pdfen
dc.relation.haspartChapt7.pdfen
dc.relation.haspartBack.pdfen
dc.relation.haspartChapt6.pdfen
dc.relation.haspartChapt3.pdfen
dc.relation.haspartFront.pdfen
dc.relation.haspartChapt2.pdfen
dc.relation.haspartChapt1.pdfen
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subjectUnsteadyen
dc.subjectcomputationsen
dc.subjectheat fluxen
dc.titleA Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impacten
dc.typeDissertationen
thesis.degree.disciplineMechanical Engineeringen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.leveldoctoralen
thesis.degree.namePh. D.en

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