Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/292961
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dc.coverage.spatial
dc.date.accessioned2020-07-28T05:30:25Z-
dc.date.available2020-07-28T05:30:25Z-
dc.identifier.urihttp://hdl.handle.net/10603/292961-
dc.description.abstractActive flow control of hypersonic flight vehicle forms a crucial design requirement for hypersonic research and technology development. Aerodynamic and propulsive controls are the two main affiliates of flow control to be achieved during flight. The flight vehicle can be a projectile, a re-entry payload, a cruise missile or an air-breathing hypersonic scramjet cruise vehicle (HSCV). Active flow control of HSCV is considered the most challenging due to complexities associated with direct coupling of hypervelocity aerodynamic and propulsive flow characteristics. For successful operation and completion of mission objectives of HSCV right from launch phase to touch-down, active flow controls which utilize new multidisciplinary and evolutionary physical mechanisms, such as electromagnetic flow control and plasma discharge flow control are required during the flight. Due to the complex interaction of electromagnetic field and chemically reacting ionized flow field, the flowfield analysis needs to consider sophisticated physical and chemical models. Hence there is a need and demand to develop a multidisciplinary numerical tool, considering the pertinent multiphysics environment for addressing research and development needs as well as for analysis of various hypersonic flow control problems. In this realm, a special purpose flow solver had been developed for addressing MHD flow control of hypersonic flight vehicles involving interaction of magnetic field and thermo-chemical non-equilibrium flowfield. This is the first time in the country that such a capability had been developed.
dc.format.extent327p.
dc.languageEnglish
dc.relation
dc.rightsuniversity
dc.titleActive flow control for hypersonic flows involving real gas and magnetohydrodynamic effects
dc.title.alternative
dc.creator.researcherBalasubramanian R
dc.subject.keywordEngineering
dc.subject.keywordEngineering and Technology
dc.subject.keywordEngineering Mechanical
dc.subject.keywordFlight vehicle
dc.subject.keywordHypersonic flows
dc.description.note
dc.contributor.guideAnandhanarayanan K
dc.publisher.placeKukatpally
dc.publisher.universityJawaharlal Nehru Technological University, Hyderabad
dc.publisher.institutionDepartment of Mechanical Engineering
dc.date.registered2008
dc.date.completed2016
dc.date.awardedMay 2016
dc.format.dimensions
dc.format.accompanyingmaterialDVD
dc.source.universityUniversity
dc.type.degreePh.D.
Appears in Departments:Faculty of Mechanical Engineering

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01_title.pdfAttached File1.13 MBAdobe PDFView/Open
02_declaration.pdf327.23 kBAdobe PDFView/Open
03_certificate.pdf583.33 kBAdobe PDFView/Open
04_acknowledgements.pdf1.33 MBAdobe PDFView/Open
05_abstract.pdf1.04 MBAdobe PDFView/Open
06_table of contents.pdf1.36 MBAdobe PDFView/Open
07_list of tables_figures_abbreviations.pdf637.78 kBAdobe PDFView/Open
08_list of publications.pdf1.07 MBAdobe PDFView/Open
09_chapter 1.pdf1.45 MBAdobe PDFView/Open
10_chapter 2.pdf1.34 MBAdobe PDFView/Open
11_chapter 3.pdf1.45 MBAdobe PDFView/Open
12_chapter 4.pdf1.41 MBAdobe PDFView/Open
13_chapter 5.pdf3.58 MBAdobe PDFView/Open
14_chapter 6.pdf4.57 MBAdobe PDFView/Open
15_chapter 7.pdf2.82 MBAdobe PDFView/Open
16_chapter 8.pdf1.88 MBAdobe PDFView/Open
17_chapter 9.pdf5.9 MBAdobe PDFView/Open
18_chapter 10.pdf1.04 MBAdobe PDFView/Open
19_appendix.pdf1.42 MBAdobe PDFView/Open
20_bibliography.pdf1.45 MBAdobe PDFView/Open
80_recommendation.pdf335.77 kBAdobe PDFView/Open


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