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dc.creatorGoy, Matthieu Pierre Bernard
dc.date.accessioned2012-06-07T22:36:29Z
dc.date.available2012-06-07T22:36:29Z
dc.date.created1994
dc.date.issued1994
dc.identifier.urihttps://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-G724
dc.descriptionDue to the character of the original source materials and the nature of batch digitization, quality control issues may be present in this document. Please report any quality issues you encounter to digital@library.tamu.edu, referencing the URI of the item.en
dc.descriptionIncludes bibliographical references.en
dc.description.abstractThe numerical simulation of a quasi one-dimensional internal flow in a subsonicsupersonic nozzle is obtained. Shocks due to high pressure ratio are computed for both inviscid and viscous flows, using an original two point subsonic-supersonic solving algorithm. Unsteady boundary consitions are considered, to simulate highly unsteady flows. The advantages of this method, in this particular case, upon a McCormack predictor-corrector scheme are developed. Comparison between the inviscid flow and the viscous flow shows that the viscous effect have little influence when the geometry of the nozzle is too large.en
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoen_US
dc.publisherTexas A&M University
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries in 2008. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en
dc.subjectmechanical engineering.en
dc.subjectMajor mechanical engineering.en
dc.titleA study of numerical methods to solve quasi one-dimensional, unsteady, compressible viscous flow with shocken
dc.typeThesisen
thesis.degree.disciplinemechanical engineeringen
thesis.degree.nameM.S.en
thesis.degree.levelMastersen
dc.type.genrethesisen
dc.type.materialtexten
dc.format.digitalOriginreformatted digitalen


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