Probabilistic aerothermal design of gas turbine combustors
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.
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| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2008
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| Online Access: | http://dspace.mit.edu/handle/1721.1/36286 http://hdl.handle.net/1721.1/36286 |
| _version_ | 1826203963169439744 |
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| author | Bradshaw, Sean D. (Sean Darien), 1978- |
| author2 | Ian Waitz. |
| author_facet | Ian Waitz. Bradshaw, Sean D. (Sean Darien), 1978- |
| author_sort | Bradshaw, Sean D. (Sean Darien), 1978- |
| collection | MIT |
| description | Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006. |
| first_indexed | 2024-09-23T12:46:41Z |
| format | Thesis |
| id | mit-1721.1/36286 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T12:46:41Z |
| publishDate | 2008 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/362862019-04-12T20:29:06Z Probabilistic aerothermal design of gas turbine combustors Bradshaw, Sean D. (Sean Darien), 1978- Ian Waitz. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006. Includes bibliographical references (p. 87-89). This thesis presents a probability-based framework for assessing the impact of manufacturing variability on combustor liner durability. Simplified models are used to link combustor liner life, liner temperature variability, and the effects of manufacturing variability. A probabilistic analysis is then applied to the simplified models to estimate the combustor life distribution. The material property and liner temperature variations accounted for approximately 80 percent and 20 percent, respectively, of the combustor life variability. Furthermore, the typical combustor life was found to be approximately 20 percent less than the life estimated using deterministic methods for these combustors, and the probability that a randomly selected combustor will fail earlier than predicted using deterministic methods is approximately 80 percent. Finally, the application of a sensitivity analysis to a surrogate model for the life identified the leading drivers of the minimum combustor life and the typical combustor life as the material property variability and the variability of the near-wall combustor gas temperature, respectively. by Sean Darien Bradshaw. Ph.D. 2008-01-10T17:32:56Z 2008-01-10T17:32:56Z 2006 2006 Thesis http://dspace.mit.edu/handle/1721.1/36286 http://hdl.handle.net/1721.1/36286 77536395 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/1721.1/36286 http://dspace.mit.edu/handle/1721.1/7582 89 p. application/pdf Massachusetts Institute of Technology |
| spellingShingle | Aeronautics and Astronautics. Bradshaw, Sean D. (Sean Darien), 1978- Probabilistic aerothermal design of gas turbine combustors |
| title | Probabilistic aerothermal design of gas turbine combustors |
| title_full | Probabilistic aerothermal design of gas turbine combustors |
| title_fullStr | Probabilistic aerothermal design of gas turbine combustors |
| title_full_unstemmed | Probabilistic aerothermal design of gas turbine combustors |
| title_short | Probabilistic aerothermal design of gas turbine combustors |
| title_sort | probabilistic aerothermal design of gas turbine combustors |
| topic | Aeronautics and Astronautics. |
| url | http://dspace.mit.edu/handle/1721.1/36286 http://hdl.handle.net/1721.1/36286 |
| work_keys_str_mv | AT bradshawseandseandarien1978 probabilisticaerothermaldesignofgasturbinecombustors |