The Effects of Particles Momentum Transfer in Shock Wave/Boundary Layer Interaction

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atmire.migration.oldid4062
dc.contributor.advisorJohansen, Craig
dc.contributor.authorTeh, E Jieh
dc.contributor.committeememberMartinuzzi, Robert
dc.contributor.committeememberBudiman, Arif
dc.contributor.committeememberLeahy, Denis
dc.date.accessioned2016-01-25T16:42:38Z
dc.date.available2016-01-25T16:42:38Z
dc.date.issued2016-01-25
dc.date.submitted2016en
dc.description.abstractNumerical simulations of solid particles seeded into a supersonic flow containing an oblique shockwave reflection were performed in order to observe and understand the momentum transfer effects between solid and gas phases in shock-wave / boundary layer interaction. Particle size and mass loading were varied to study the problem. It was found that solid particles were capable of significant modulation of the flow field as the separation bubble was suppressed primarily by the additional momentum introduced by the particles into the flow field. The particle size controlled the rate of momentum transfer while the particle mass loading controlled the magnitude of momentum transfer. As particles are seeded into the flow, a flow transition to unsteady, three-dimensional flow is observed in the simulations. The seeding of micro and nano-particle upstream of a supersonic air-breathing propulsion system as a flow control concept is proposed.en_US
dc.identifier.citationTeh, E. J. (2016). The Effects of Particles Momentum Transfer in Shock Wave/Boundary Layer Interaction (Master's thesis, University of Calgary, Calgary, Canada). Retrieved from https://prism.ucalgary.ca. doi:10.11575/PRISM/28111en_US
dc.identifier.doihttp://dx.doi.org/10.11575/PRISM/28111
dc.identifier.urihttp://hdl.handle.net/11023/2774
dc.language.isoeng
dc.publisher.facultyGraduate Studies
dc.publisher.institutionUniversity of Calgaryen
dc.publisher.placeCalgaryen
dc.rightsUniversity of Calgary graduate students retain copyright ownership and moral rights for their thesis. You may use this material in any way that is permitted by the Copyright Act or through licensing that has been assigned to the document. For uses that are not allowable under copyright legislation or licensing, you are required to seek permission.
dc.subjectEngineering--Aerospace
dc.subjectEngineering--Mechanical
dc.subject.classificationShock Waveen_US
dc.subject.classificationMultiphaseen_US
dc.subject.classificationDusty Gasen_US
dc.subject.classificationSupersonic Flowen_US
dc.subject.classificationCompressible Flowen_US
dc.subject.classificationFlow Controlen_US
dc.subject.classificationBoundary layer separationen_US
dc.titleThe Effects of Particles Momentum Transfer in Shock Wave/Boundary Layer Interaction
dc.typemaster thesis
thesis.degree.disciplineMechanical and Manufacturing Engineering
thesis.degree.grantorUniversity of Calgary
thesis.degree.nameMaster of Science (MSc)
ucalgary.item.requestcopytrue
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