Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/483466
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dc.coverage.spatialMechanical Engineering
dc.date.accessioned2023-05-16T05:15:30Z-
dc.date.available2023-05-16T05:15:30Z-
dc.identifier.urihttp://hdl.handle.net/10603/483466-
dc.description.abstractShock wave boundary layer interaction SWBLI is a classical example of viscous inviscid interactions Occurrence of SWBLI in hypersonic flowfield is extremely adverse for the space missions and needs thorough investigations Enhanced surface heating alteration in aerodynamic coefficients vortex shedding etc are the possible reasons for this consideration In view of this numerical studies are planned to enhance the understanding about this interaction However these investigations demand a
dc.format.extentNot Available
dc.languageEnglish
dc.relationNot Available
dc.rightsself
dc.titleNumerical investigations of shock wave boundary layer interaction in hypersonic flows
dc.title.alternativeNot available
dc.creator.researcherJohn, Bibin
dc.subject.keywordEngineering
dc.subject.keywordEngineering and Technology
dc.subject.keywordEngineering Mechanical
dc.description.noteNot Available
dc.contributor.guideKulkarni, Vinayak
dc.publisher.placeGuwahati
dc.publisher.universityIndian Institute of Technology Guwahati
dc.publisher.institutionDEPARTMENT OF MECHANICAL ENGINEERING
dc.date.registered2009
dc.date.completed2014
dc.date.awarded2014
dc.format.dimensionsNot Available
dc.format.accompanyingmaterialNone
dc.source.universityUniversity
dc.type.degreePh.D.
Appears in Departments:DEPARTMENT OF MECHANICAL ENGINEERING

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