Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/420620
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dc.coverage.spatialMechanical Engineering
dc.date.accessioned2022-11-25T12:24:20Z-
dc.date.available2022-11-25T12:24:20Z-
dc.identifier.urihttp://hdl.handle.net/10603/420620-
dc.description.abstractHigher wave drag is a common problem for an object flying in the supersonic or hypersonic flow regime Hence the present investigations use computational fluid dynamics as a tool to study the dynamics of flow field to mitigate the adverse effects in such a complex environment For this a finite volume based two dimensional axisymmetric compressible reacting flow solver is developed which is comprised of five species and eleven chemical elementary reactions Initial investigations on blunt obje...
dc.format.extentNot Available
dc.languageEnglish
dc.relationNot Available
dc.rightsself
dc.titleAerothermodynamic analysis of flow modification techniques in non equilibrium supersonic hypersonic flows
dc.title.alternativeNot available
dc.creator.researcherKumar, Shailendra
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.registered2016
dc.date.completed2021
dc.date.awarded2021
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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