Nonlinear aircraft engine model for future integrated power center development
Aircraft engines, the prime source of on-board power, play a vital role within the electrical power generation system. In literature these are considerably simplified to rudimentary engine speed. In this paper, a nonlinear zero-dimension (0-D) order turbofan engine model has been developed for use w...
| Main Authors: | , , , , |
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| Format: | Conference or Workshop Item |
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2016
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| Online Access: | https://eprints.nottingham.ac.uk/38777/ |
| _version_ | 1848795688828141568 |
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| author | Enalou, H.B. Rashed, Mohamed Kulsangcharoen, Ponggorn Hill, Christopher Ian Bozhko, Serhiy |
| author_facet | Enalou, H.B. Rashed, Mohamed Kulsangcharoen, Ponggorn Hill, Christopher Ian Bozhko, Serhiy |
| author_sort | Enalou, H.B. |
| building | Nottingham Research Data Repository |
| collection | Online Access |
| description | Aircraft engines, the prime source of on-board power, play a vital role within the electrical power generation system. In literature these are considerably simplified to rudimentary engine speed. In this paper, a nonlinear zero-dimension (0-D) order turbofan engine model has been developed for use with an integrated power center. By analyzing the compressor maps in detail, the results reveal a limit on the amount power off-take from each engine shaft at different altitudes. |
| first_indexed | 2025-11-14T19:36:04Z |
| format | Conference or Workshop Item |
| id | nottingham-38777 |
| institution | University of Nottingham Malaysia Campus |
| institution_category | Local University |
| last_indexed | 2025-11-14T19:36:04Z |
| publishDate | 2016 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | nottingham-387772020-05-04T18:12:53Z https://eprints.nottingham.ac.uk/38777/ Nonlinear aircraft engine model for future integrated power center development Enalou, H.B. Rashed, Mohamed Kulsangcharoen, Ponggorn Hill, Christopher Ian Bozhko, Serhiy Aircraft engines, the prime source of on-board power, play a vital role within the electrical power generation system. In literature these are considerably simplified to rudimentary engine speed. In this paper, a nonlinear zero-dimension (0-D) order turbofan engine model has been developed for use with an integrated power center. By analyzing the compressor maps in detail, the results reveal a limit on the amount power off-take from each engine shaft at different altitudes. 2016-09-09 Conference or Workshop Item PeerReviewed Enalou, H.B., Rashed, Mohamed, Kulsangcharoen, Ponggorn, Hill, Christopher Ian and Bozhko, Serhiy (2016) Nonlinear aircraft engine model for future integrated power center development. In: ESARS Itec 2016, 2-4 Nov 2016, Toulouse, France. Turbofan Modeling power off-take |
| spellingShingle | Turbofan Modeling power off-take Enalou, H.B. Rashed, Mohamed Kulsangcharoen, Ponggorn Hill, Christopher Ian Bozhko, Serhiy Nonlinear aircraft engine model for future integrated power center development |
| title | Nonlinear aircraft engine model for future integrated power center development |
| title_full | Nonlinear aircraft engine model for future integrated power center development |
| title_fullStr | Nonlinear aircraft engine model for future integrated power center development |
| title_full_unstemmed | Nonlinear aircraft engine model for future integrated power center development |
| title_short | Nonlinear aircraft engine model for future integrated power center development |
| title_sort | nonlinear aircraft engine model for future integrated power center development |
| topic | Turbofan Modeling power off-take |
| url | https://eprints.nottingham.ac.uk/38777/ |