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Please use this identifier to cite or link to this item: http://142.54.178.187:9060/xmlui/handle/123456789/1717
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dc.contributor.authorAtta Ullah-
dc.contributor.authorNadeem, Muhammad-
dc.contributor.authorAhmed, Asif Nazir-
dc.date.accessioned2019-11-21T11:30:11Z-
dc.date.available2019-11-21T11:30:11Z-
dc.date.issued2009-10-19-
dc.identifier.isbn978-1-4244-5630-7-
dc.identifier.urihttp://142.54.178.187:9060/xmlui/handle/123456789/1717-
dc.description.abstractThis paper consists of theoretical modeling and computer simulation of two phase isothermal flow in a convergent divergent nozzle. First general expressions to determine velocity at any point, velocity at throat and speed of sound for two phase isothermal flow through convergent divergent nozzle as a function of pressure and initial volume ratio are developed using basic laws of energy, momentum and ideal gas equation. Then continuity equation is used to derive an expression for area ratio. By using these expressions data is generated for various values of initial volume ratios. Variation in Mach number ratio, velocity ratio, volume ratio, density ratio, pressure ratio with change in area ratio is also observed. A comparison of analytical results with experimental data shows minor deviations. The model developed can be applied to all realistic isothermal compressible two phase flows.en_US
dc.language.isoen_USen_US
dc.publisherIEEE 2009 International Conference on Emerging Technologiesen_US
dc.subjectEngineering and Technologyen_US
dc.subjectModelingen_US
dc.subjectTwo phase flowen_US
dc.subjectConvergent- divergent nozzleen_US
dc.titleModeling of two phase flow in a convergent- divergent nozzleen_US
dc.typeProceedingsen_US
Appears in Collections:Proceedings

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