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A study of the vortex sheet behind a lifting wing.Williams, David Prior. January 1976 (has links) (PDF)
Thesis (M.Sc.) -- University of Adelaide, Dept. of Applied Mathematics, 1977.
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Three dimensional flow analysis by the vortex-lattice method /Rodriguez, Carlos Guillermo, January 1990 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1990. / Vita. Abstract. Includes bibliographical references (leaves 45-46). Also available via the Internet.
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Investigation of reversal phenomena in forebody vortex manipulation by forward facing nozzles /Neuteboom, Martin January 1900 (has links)
Thesis (M.App.Sc.) - Carleton University, 2003. / Includes bibliographical references (p. 74-75).
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Numerical simulations of diffusing s-duct and vortex-generator-jet flows.Grosvenor, Allan D., January 1900 (has links)
Thesis (M. Eng.)--Carleton University, 2000. / Also available in electronic format on the Internet.
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Fluid nonlinearities for calibrated VIV wake oscillator modelsKurishina, Victoria January 2018 (has links)
Onshore and offshore structures are subject of strict safety regulations, and acceptable design implies requirements for accurate models of potentially dangerous phenomena. The phenomenon of Vortex-Induced Vibrations (VIVs) develops when a slender structure interacts with a fluid flow. Vortices grow in the disturbed boundary layer and spread behind the structure, resulting in fluctuations of the fluid forces acting on the body. Slender structures are present almost everywhere in the form of tall buildings and skyscrapers, cranes, antennas, power lines, suspension bridges, umbilicals, risers and free spans of pipelines which deliver water, oil and gas. The deeper in the water and higher in the sky these structures are, more likely they can experience VIVs and the lock-in state due to the exposure to various flow profiles. The wake oscillator method allows to model fluid variables during VIV lock-in using self-excited and self-limited oscillators of Van der Pol or Rayleigh type. In this research, the capabilities of alternative nonlinear oscillators as fluid equations are considered for modelling elastically supported rigid structures with one and two degrees-of-freedom in uniform flow. For modelling two-dimensional flexible structures in uniform and sheared flows, new wake oscillator models are developed in this work and applied with alternative damping terms. The dynamics of the uniform flow model of flexible structure is investigated in detail with the focus on coexisting solutions of the displacement amplitudes. Empirical coefficients for wake oscillator models are calibrated in this study using constrained nonlinear minimization and experimental data available in the literature. The validation performed confirms the most successful results for the suite of models of 2DOF rigid structure for low mass ratio, where agreement with both in-line and cross-flow displacement records was obtained.
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Large-eddy simulation of a three-dimensional compressible tornado vortexXia, Jianjun. January 2001 (has links)
Thesis (Ph. D.)--West Virginia University, 2001. / Title from document title page. Document formatted into pages; contains xviii, 130 p. : ill. (some col.). Vita. Includes abstract. Includes bibliographical references (p. 98-104).
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Near wake flow interactions of two square cylinders /Chiu, Yuen-wang, Alex. January 1999 (has links)
Thesis (Ph. D.)--University of Hong Kong, 1999. / Includes bibliographical references (leaves 211-243).
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On the stability and propagation of barotropic modons in slowly varying mediaSwaters, Gordon Edwin, January 1985 (has links)
Thesis (Ph. D.)--University of British Columbia, 1985. / Includes bibliographical references (leaves 120-125).
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Numerical simulations of turbulent flows /Johansen, Craig T., January 1900 (has links)
Thesis (M.App.Sc.) - Carleton University, 2005. / Includes bibliographical references (p. 224-244). Also available in electronic format on the Internet.
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