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Transonic similarity solution for aligned field MHD nozzle flow
dc.contributor.authorWatanabe, H.en_US
dc.contributor.authorSichel, Martinen_US
dc.contributor.authorOng, Rudi Siong Bweeen_US
dc.date.accessioned2006-09-08T20:37:47Z
dc.date.available2006-09-08T20:37:47Z
dc.date.issued1973-04en_US
dc.identifier.citationWatanabe, H.; Sichel, M.; Ong, R. S. B.; (1973). "Transonic similarity solution for aligned field MHD nozzle flow." Journal of Engineering Mathematics 7(2): 127-137. <http://hdl.handle.net/2027.42/42703>en_US
dc.identifier.issn0022-0833en_US
dc.identifier.issn1573-2703en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/42703
dc.description.abstractThe transonic flow near the throat of a converging-diverging nozzle of a gas with infinite electrical conductivity is considered. The magnetic field B is everywhere aligned with the velocity q so that the equations describing the flow are reducible to those of ordinary gasdynamics. Thus, it is possible to utilize the transonic similarity solution of Tomotika and Tamada [3] to study aligned field magnetohydrodynamic flow near a nozzle throat. Only transonic flows are considered, and the structures of sub- and supersonic flows with speeds greater and less than the Alfvén speed are investigated.en_US
dc.format.extent643740 bytes
dc.format.extent3115 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.language.isoen_US
dc.publisherKluwer Academic Publishers; Noordhoff International Publishing ; Springer Science+Business Mediaen_US
dc.subject.otherPhysicsen_US
dc.subject.otherNumeric Computingen_US
dc.subject.otherAnalysisen_US
dc.subject.otherApplications of Mathematicsen_US
dc.subject.otherMathematical Modeling and Industrial Mathematicsen_US
dc.subject.otherMechanicsen_US
dc.titleTransonic similarity solution for aligned field MHD nozzle flowen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelEngineering (General)en_US
dc.subject.hlbsecondlevelMechanical Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumDepartment of Aerospace Engineering, The University of Michigan, Ann Arbor, Michigan, USAen_US
dc.contributor.affiliationumDepartment of Aerospace Engineering, The University of Michigan, Ann Arbor, Michigan, USAen_US
dc.contributor.affiliationumDepartment of Aerospace Engineering, The University of Michigan, Ann Arbor, Michigan, USAen_US
dc.contributor.affiliationumcampusAnn Arboren_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/42703/1/10665_2005_Article_BF01535358.pdfen_US
dc.identifier.doihttp://dx.doi.org/10.1007/BF01535358en_US
dc.identifier.sourceJournal of Engineering Mathematicsen_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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