Structural and dynamic differences in the turbulent wake of cantilevered square and circular cylinders protruding a thin laminar boundary layer

dc.contributor.advisorMartinuzzi, Robert John
dc.contributor.authorKindree, Matthew Gordon
dc.contributor.committeememberWood, David H.
dc.contributor.committeememberKorobenko, Artem
dc.contributor.committeememberHassanzadeh, Hassan
dc.date2019-11
dc.date.accessioned2019-08-16T21:28:50Z
dc.date.available2019-08-16T21:28:50Z
dc.date.issued2019-08-16
dc.description.abstractThis thesis documents a comparative experimental study of the vortical structures and dynamics in the turbulent wake of aspect ratio 4 cantilevered square and circular cylinders at a Reynolds number of 10500 protruding a thin laminar boundary layer. Antisymmetric Kármán-like vortex shedding of half-loop structures is observed in the phase-averaged field of both cylinders. The signature of these shed vortices are dipole structures imprinted on the mean wakes. The half-loop structures, associated spectral signatures, and dipole vortices are concentrated at lower elevations in the circular cylinder wake but span the square cylinder’s entire height and are significantly stronger. A low-frequency instability is observed at high elevations of both cylinder wakes but at different frequencies and is more broadband for the square cylinder. The low frequency signature spans the entire height of the square cylinder and therefore interacts with the vortex shedding. Both low-frequency signatures are shown to be unique to laminar boundary layers. However, these cannot be directly related to instabilities of the laminar horseshoe vortex system. The square cylinder exhibits a significantly more complex mean wake structure with vortices descending from the dipole pair and growing from the ground plate into the far wake. Increased bluffness of the square cylinder geometry leads to stronger rotation of merging structures in the phase-averaged field and formation of these additional mean wake structures. Furthermore, a vortex along the ground plate forms in the mean field of both cylinders which is the signature of a complex interaction between the primary horseshoe vortex legs and the shedding structures. Above the cylinder free-ends, both cylinders exhibit tip vortices planted to their free-end surface that extend into the near wake region. These tip vortices are mostly steady for the circular cylinder but oscillate vertically at the vortex shedding frequency for the square cylinder. Thus, the square cylinder’s free-end flow directly interacts with the vortex shedding in the wake. This work establishes that square and circular cylinder geometries give rise to topologically and dynamically distinct wakes and that the boundary layer state influences the dynamics.en_US
dc.identifier.citationKindree, M. G. (2019). Structural and dynamic differences in the turbulent wake of cantilevered square and circular cylinders protruding a thin laminar boundary layer (Master's thesis, University of Calgary, Calgary, Canada). Retrieved from https://prism.ucalgary.ca.en_US
dc.identifier.doihttp://dx.doi.org/10.11575/PRISM/36818
dc.identifier.urihttp://hdl.handle.net/1880/110727
dc.language.isoengen_US
dc.publisher.facultySchulich School of Engineeringen_US
dc.publisher.institutionUniversity of Calgaryen
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.en_US
dc.subjectVortex Sheddingen_US
dc.subjectCantilevered Bluff Bodiesen_US
dc.subjectParticle Image Velocimetryen_US
dc.subjectTurbulent Wake Flowsen_US
dc.subjectHorseshoe Vortex Systemen_US
dc.subjectTip Flowsen_US
dc.subjectLaminar Boundary Layersen_US
dc.subjectLow Frequency Wake Dynamicsen_US
dc.subject.classificationEngineering--Mechanicalen_US
dc.titleStructural and dynamic differences in the turbulent wake of cantilevered square and circular cylinders protruding a thin laminar boundary layeren_US
dc.typemaster thesisen_US
thesis.degree.disciplineEngineering – Mechanical & Manufacturingen_US
thesis.degree.grantorUniversity of Calgaryen_US
thesis.degree.nameMaster of Science (MSc)en_US
ucalgary.item.requestcopytrueen_US
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