{"id":{"repo_id":"gatech","oai_identifier":"oai:repository.gatech.edu:1853/26605"},"canonical_url":"https://search.dev.ndltd.org/etd/gatech/oai:repository.gatech.edu:1853/26605","repository":{"repo_id":"gatech","name":"Georgia Tech","base_url":"https://repository.gatech.edu/server/oai/request"},"display":{"title":"Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion","abstract":"The main objective of this thesis is to develop a comprehensive model with the capability of modeling both a high Reynolds number and high magnetic Reynolds number turbulent flow for application to supersonic combustor. The development of this model can be divided into three categories: one, the development of a self-consistent MHD numerical model capable of modeling magnetic turbulence in high magnetic Reynolds number applications. Second, the development of a gas discharge model which models the interaction of externally applied fields in conductive medium. Third, the development of models necessary for studying supersonic combustion applications with plasma-assistance such the extension of chemical kinetics models to extremely high temperature and non-equilibrium phenomenon.","abstract_html":"The main objective of this thesis is to develop a comprehensive model with the capability of modeling both a high Reynolds number and high magnetic Reynolds number turbulent flow for application to supersonic combustor. The development of this model can be divided into three categories: one, the development of a self-consistent MHD numerical model capable of modeling magnetic turbulence in high magnetic Reynolds number applications. Second, the development of a gas discharge model which models the interaction of externally applied fields in conductive medium. Third, the development of models necessary for studying supersonic combustion applications with plasma-assistance such the extension of chemical kinetics models to extremely high temperature and non-equilibrium phenomenon.","abstract_has_math":false,"creators":["Miki, Kenji"],"institution":"Georgia Institute of Technology","degree_name":null,"degree_level":null,"degree_discipline":null,"degree_department":"Aerospace Engineering","school":null,"contributors":[],"advisors":["Menon, Suresh","Jagoda, Jechiel I."],"committee_chairs":[],"committee_members":["Ruffin, Stephen M.","Stoesser, Thorsten","Walker, Mitchell L."],"year":2009,"date_issued":"2009-01-14","date_published":"2009-01-14","updated_at":"2026-07-27T19:49:46Z","subjects":["Scramjet","MHD","Turbulence","Supersonic flow","Plasma"],"languages":[],"rights":[],"rights_urls":[],"identifier_entries":[]},"links":{"outbound_url":"http://hdl.handle.net/1853/26605","outbound_label":"Handle","outbound_source":"dc:identifier.uri"},"metadata_groups":[{"id":"people","label":"People","entries":[{"key":"dc:contributor.advisor","label":"Advisor","values":["Menon, Suresh","Jagoda, Jechiel I."]},{"key":"dc:contributor.committeemember","label":"Committee Member","values":["Ruffin, Stephen M.","Stoesser, Thorsten","Walker, Mitchell L."]},{"key":"dc:contributor.department","label":"Department","values":["Aerospace Engineering"]},{"key":"dc:creator","label":"Author","values":["Miki, Kenji"]}]},{"id":"academic_context","label":"Academic Context","entries":[{"key":"dc:date.accessioned","label":"Dc Date Accessioned","values":["2009-01-22T15:49:40Z"]},{"key":"dc:date.available","label":"Dc Date Available","values":["2009-01-22T15:49:40Z"]},{"key":"dc:date.issued","label":"Date","values":["2009-01-14"]},{"key":"dc:publisher","label":"Institution","values":["Georgia Institute of Technology"]},{"key":"dc:type","label":"Dc Type","values":["Text"]}]},{"id":"subjects_keywords","label":"Subjects and Keywords","entries":[{"key":"dc:subject","label":"Dc Subject","values":["Scramjet","MHD","Turbulence","Supersonic flow","Plasma"]}]},{"id":"identifiers","label":"Identifiers","entries":[{"key":"dc:identifier.uri","label":"Identifier URI","values":["http://hdl.handle.net/1853/26605"]}]},{"id":"additional","label":"Additional Metadata","entries":[{"key":"dc:description.abstract","label":"Abstract","values":["The main objective of this thesis is to develop a comprehensive model with the capability of modeling both a high Reynolds number and high magnetic Reynolds number turbulent flow for application to supersonic combustor. The development of this model can be divided into three categories: one, the development of a self-consistent MHD numerical model capable of modeling magnetic turbulence in high magnetic Reynolds number applications. Second, the development of a gas discharge model which models the interaction of externally applied fields in conductive medium. Third, the development of models necessary for studying supersonic combustion applications with plasma-assistance such the extension of chemical kinetics models to extremely high temperature and non-equilibrium phenomenon."]},{"key":"dc:description.degree","label":"Dc Description Degree","values":["Ph.D."]},{"key":"dc:title","label":"Title","values":["Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion"]}]}],"canonical_facts":{"dc:contributor.advisor":["Menon, Suresh","Jagoda, Jechiel I."],"dc:contributor.committeemember":["Ruffin, Stephen M.","Stoesser, Thorsten","Walker, Mitchell L."],"dc:contributor.department":["Aerospace Engineering"],"dc:creator":["Miki, Kenji"],"dc:date.accessioned":["2009-01-22T15:49:40Z"],"dc:date.available":["2009-01-22T15:49:40Z"],"dc:date.issued":["2009-01-14"],"dc:description.abstract":["The main objective of this thesis is to develop a comprehensive model with the capability of modeling both a high Reynolds number and high magnetic Reynolds number turbulent flow for application to supersonic combustor. 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