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dc.contributor.advisorDey, J
dc.contributor.authorKumar, P Phani
dc.date.accessioned2018-06-23T12:08:37Z
dc.date.accessioned2018-07-31T05:16:42Z
dc.date.available2018-06-23T12:08:37Z
dc.date.available2018-07-31T05:16:42Z
dc.date.issued2018-06-23
dc.date.submitted2016
dc.identifier.urihttp://etd.iisc.ac.in/handle/2005/3749
dc.identifier.abstracthttp://etd.iisc.ac.in/static/etd/abstracts/4620/G28436-Abs.pdfen_US
dc.description.abstractA high level of free-stream turbulence and surface roughness are known to cause breakdown of an otherwise stable laminar flow. In transition induced by free-stream turbulence, streaks are formed due to the lift-up effect and low-speed streaks with high shear breakdown to turbulence. Streaks are also present in transition caused by a roughness element and they may breakdown via sinuous or varicose instability. In general, streamwise streaks, their lift-up and streak instability are integral to the bypass transition process. If the lift-up of a high-shear layer or its breakdown is manipulated by some external means, then the downstream flow is expected to change. An experimental study was carried out to understand the effect of flow modification caused by a mesh placed normal to the flow and at different wall-normal locations in the late stage of bypass transitions induced separately by an isolated cylindrical roughness element and a high level of free-stream turbulence. The measurements were made on a flat plate boundary layer in a low-speed wind tunnel using the particle image velocimetry technique. The mesh causes an approximately 30% reduction in the free-stream velocity, and mild acceleration in the boundary layer, irrespective of its wall-normal location. Interestingly, when located near the wall, the mesh suppresses several transitional events leading to transition delay over a large downstream distance. The transition delay is found to be mainly caused by suppression of the lift-up of the high-shear layer and its distortion, along with modification of the spanwise streaky structure to an orderly one. However, with the mesh well away from the wall, the lifted-up shear layer remains largely unaffected, and the downstream boundary layer velocity profile develops an overshoot which is found to follow a plane mixing layer type profile up to the free stream. Reynolds stresses, and the size and strength of vortices increase in this mixing layer region. The high-intensity disturbance in this region can possibly enhance the transition of accelerated flow far downstream, although a reduction in streamwise turbulence intensity occurs over a short distance downstream of the mesh. However, the shape of large-scale streamwise structure in the wall-normal plane is found to be more or less the same as that without the mesh.en_US
dc.language.isoen_USen_US
dc.relation.ispartofseriesG28436en_US
dc.subjectBoundary Layer Transitionen_US
dc.subjectFree-stream Turbulenceen_US
dc.subjectIsolated Roughness Elementen_US
dc.subjectLaminar Flowen_US
dc.subject.classificationAerospace Engineeringen_US
dc.titleEffect of a Mesh on Boundary Layer Transition Induced by Free-stream Turbulence and an Isolated Roughness Elementen_US
dc.typeThesisen_US
dc.degree.namePhDen_US
dc.degree.levelDoctoralen_US
dc.degree.disciplineFaculty of Engineeringen_US


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