A method for propulsion nozzle design

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dc.contributor.authorEskandarian, Azimen
dc.contributor.departmentMechanical Engineeringen
dc.date.accessioned2020-12-15T19:11:33Zen
dc.date.available2020-12-15T19:11:33Zen
dc.date.issued1983en
dc.description.abstractAn inverse method for the design of exhaust nozzles with a specified transonic pressure distribution is presented. A problem of mixed Neumann and Dirichlet boundary condition is solved. A successive line relaxation process is used to solve the array of velocity potentials in the entire flow field. The streamlines are then displaced to produce boundaries which match a desired pressure distribution. Various cases are tested to verify the reliability of the method. The design calculation proves to be efficient and accurate.en
dc.description.degreeM.S.en
dc.format.extentx, 58 leavesen
dc.format.mimetypeapplication/pdfen
dc.identifier.urihttp://hdl.handle.net/10919/101430en
dc.language.isoenen
dc.publisherVirginia Polytechnic Institute and State Universityen
dc.relation.isformatofOCLC# 11069729en
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V855 1983.E842en
dc.subject.lcshAerodynamics, Transonicen
dc.subject.lcshJet nozzlesen
dc.titleA method for propulsion nozzle designen
dc.typeThesisen
dc.type.dcmitypeTexten
thesis.degree.disciplineMechanical Engineeringen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.levelmastersen
thesis.degree.nameM.S.en

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