Vortex driven flame dynamics and combustion instability
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2005.
| मुख्य लेखक: | |
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| अन्य लेखक: | |
| स्वरूप: | थीसिस |
| भाषा: | eng |
| प्रकाशित: |
Massachusetts Institute of Technology
2006
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| विषय: | |
| ऑनलाइन पहुंच: | http://hdl.handle.net/1721.1/32379 |
| _version_ | 1826198114478850048 |
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| author | Altay, Hurrem Murat |
| author2 | Ahmed F. Ghoniem. |
| author_facet | Ahmed F. Ghoniem. Altay, Hurrem Murat |
| author_sort | Altay, Hurrem Murat |
| collection | MIT |
| description | Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2005. |
| first_indexed | 2024-09-23T10:59:04Z |
| format | Thesis |
| id | mit-1721.1/32379 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T10:59:04Z |
| publishDate | 2006 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/323792022-01-13T07:54:36Z Vortex driven flame dynamics and combustion instability Altay, Hurrem Murat Ahmed F. Ghoniem. Massachusetts Institute of Technology. Dept. of Mechanical Engineering. Massachusetts Institute of Technology. Department of Mechanical Engineering Mechanical Engineering. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2005. Includes bibliographical references (leaves 87-93). Combustion instability in premixed combustors mostly arises due to the coupling between heat release rate dynamics and system acoustics. It is crucial to understand the instability mechanisms to design reliable, high efficiency, low emission gas turbine combustors. In this thesis, elementary processes acting as a source of unsteady heat release rate are described. These elementary processes are acoustic wave-flame interactions, flame-vortex interactions, equivalence ratio fluctuations, flame-wall interactions and the unsteady stretch rate. To investigate the flame- vortex interaction mechanism, a parametric study is performed in single and double expansion dump combustors. 2-D simulations are performed using the random vortex method combined with thin flame model of premixed combustion. The inlet velocity of the combustor is forced sinusoidally at various amplitudes and frequencies, and the heat release rate response is evaluated. It is shown that the heat release rate dynamics are governed by the cyclical formation of a large wake vortex and its interaction with the flame. Maximum heat release rate in a cycle is reached a short time after the breakup of the vortex, which causes rapid burning of the reactants trapped within the structure. The geometry and operating conditions of the combustor control the mechanism by which the vortex breakup is initiated. For short cavities, the impingement of the large wake vortex onto the forward facing step is responsible from the vortex breakup. (cont.) On the other hand, in long cavities, the vortex breakup is initiated as the wake vortex impinges on the upper cavity wall in single expansion dump combustor, or the vortex forming in the other half of the combustor in double expansion dump combustor. Furthermore, the effect of the air injection in the cross stream direction close to the dump plane on equivalence ratio is investigated. It is shown experimentally that high amplitude pressure oscillation in the combustor during unstable operation causes fluctuation in the injected jet velocity. The oscillatory jet velocity affects the incoming equivalence ratio depending on the momentum ratio of the jet to the primary stream. A critical momentum ratio is defined at which the amplitude of the equivalence ratio oscillations reaches a maximum. by Hurrem Murat Altay. S.M. 2006-03-29T18:39:10Z 2006-03-29T18:39:10Z 2005 2005 Thesis http://hdl.handle.net/1721.1/32379 61522832 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 93 leaves 5106557 bytes 5111076 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology |
| spellingShingle | Mechanical Engineering. Altay, Hurrem Murat Vortex driven flame dynamics and combustion instability |
| title | Vortex driven flame dynamics and combustion instability |
| title_full | Vortex driven flame dynamics and combustion instability |
| title_fullStr | Vortex driven flame dynamics and combustion instability |
| title_full_unstemmed | Vortex driven flame dynamics and combustion instability |
| title_short | Vortex driven flame dynamics and combustion instability |
| title_sort | vortex driven flame dynamics and combustion instability |
| topic | Mechanical Engineering. |
| url | http://hdl.handle.net/1721.1/32379 |
| work_keys_str_mv | AT altayhurremmurat vortexdrivenflamedynamicsandcombustioninstability |