Feedback control of separation in unsteady flows
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2005.
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| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2006
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| Online Access: | http://hdl.handle.net/1721.1/32377 |
| _version_ | 1826189658342555648 |
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| author | Alam, Mohammad-Reza |
| author2 | George Haller. |
| author_facet | George Haller. Alam, Mohammad-Reza |
| author_sort | Alam, Mohammad-Reza |
| collection | MIT |
| description | Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2005. |
| first_indexed | 2024-09-23T08:19:06Z |
| format | Thesis |
| id | mit-1721.1/32377 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T08:19:06Z |
| publishDate | 2006 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/323772019-04-09T17:55:11Z Feedback control of separation in unsteady flows Alam, Mohammad-Reza George Haller. Massachusetts Institute of Technology. Dept. of Mechanical Engineering. Massachusetts Institute of Technology. Dept. of Mechanical Engineering. Mechanical Engineering. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2005. Includes bibliographical references (leaves 67-69). Prandtl (1904) showed that in a steady flow past a bluff body, streamlines separate from the boundary where the skin friction (or wall shear) vanishes and admits a negative gradient. Despite initial suggestions, however, it was recognized that Prandtl's zero-skin-friction criterion for separation is invalid for unsteady flows. Employing a Lagrangian approach, Haller (2004) derived an exact kinematic theory for unsteady separation in two-dimensional flows. This theory predicts separation at points where a weighted average of the skin-friction vanishes. The weight function in this criterion depends on quantities measured along the wall, and hence can be used in an active feedback control of separation. Feedback control has been shown to lead to performance improvement in a range of aerodynamic applications, but no rigorous feedback law has been constructed for lack of a detailed understanding of separation. In this work, we use a wall-reduced form of the vorticity-transport equation to design a feedback controller that enforces Haller's criteria-and hence induces separation- at prescribed boundary points. We also present a stability analysis of the controller, and explore alternative control strategies for separation. We use FLUENT to validate our controller numerically on a range of flows, including steady and unsteady channel flows and backward-facing step flows. by Mohammad-Reza. S.M. 2006-03-29T18:38:59Z 2006-03-29T18:38:59Z 2005 2005 Thesis http://hdl.handle.net/1721.1/32377 61516475 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 86 leaves 3384825 bytes 3388709 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology |
| spellingShingle | Mechanical Engineering. Alam, Mohammad-Reza Feedback control of separation in unsteady flows |
| title | Feedback control of separation in unsteady flows |
| title_full | Feedback control of separation in unsteady flows |
| title_fullStr | Feedback control of separation in unsteady flows |
| title_full_unstemmed | Feedback control of separation in unsteady flows |
| title_short | Feedback control of separation in unsteady flows |
| title_sort | feedback control of separation in unsteady flows |
| topic | Mechanical Engineering. |
| url | http://hdl.handle.net/1721.1/32377 |
| work_keys_str_mv | AT alammohammadreza feedbackcontrolofseparationinunsteadyflows |