Optimum Turbofan Engine Performance Through Variation of Bypass Ratio
The desire for higher engine efficiency has resulted in the evolution of aircraft gas turbine engines from turbojets, to low bypass ratio, first generation turbofans, to today’s high bypass ratio turbofans. It is possible that future designs will continue this trend, leading to very-high or ultra...
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| Format: | Article |
| Language: | Arabic |
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Mustansiriyah University/College of Engineering
2013-03-01
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| Series: | Journal of Engineering and Sustainable Development |
| Subjects: | |
| Online Access: | https://jeasd.uomustansiriyah.edu.iq/index.php/jeasd/article/view/1097 |
| _version_ | 1798022543161950208 |
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| author | Marwan Fakhri Basher |
| author_facet | Marwan Fakhri Basher |
| author_sort | Marwan Fakhri Basher |
| collection | DOAJ |
| description |
The desire for higher engine efficiency has resulted in the evolution of aircraft gas turbine engines from turbojets, to low bypass ratio, first generation turbofans, to today’s high bypass ratio turbofans. It is possible that future designs will continue this trend, leading to very-high or ultra-high bypass ratio engines . The most significant impact of the design changes was a reduction in the aircraft weight and block fuel penalties incurred with low fan pressure ratio, ultra-high bypass ratio designs. This enables lower noise levels to be pursued (through lower fan pressure ratio) with minor negative impacts on aircraft weight and fuel efficiency. Regardless of the engine design selected, the results of this study indicate the potential for the advanced aircraft to realize substantial improvements in fuel efficiency, emissions, and noise compared to the current engines in this size class
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| first_indexed | 2024-04-11T17:31:45Z |
| format | Article |
| id | doaj.art-ea455c8958724a00bad2740845fd9cef |
| institution | Directory Open Access Journal |
| issn | 2520-0917 2520-0925 |
| language | Arabic |
| last_indexed | 2024-04-11T17:31:45Z |
| publishDate | 2013-03-01 |
| publisher | Mustansiriyah University/College of Engineering |
| record_format | Article |
| series | Journal of Engineering and Sustainable Development |
| spelling | doaj.art-ea455c8958724a00bad2740845fd9cef2022-12-22T04:12:00ZaraMustansiriyah University/College of EngineeringJournal of Engineering and Sustainable Development2520-09172520-09252013-03-01171Optimum Turbofan Engine Performance Through Variation of Bypass RatioMarwan Fakhri Basher0Department of Mechanical Engineering, University of Mosul, Ninawa, Iraq The desire for higher engine efficiency has resulted in the evolution of aircraft gas turbine engines from turbojets, to low bypass ratio, first generation turbofans, to today’s high bypass ratio turbofans. It is possible that future designs will continue this trend, leading to very-high or ultra-high bypass ratio engines . The most significant impact of the design changes was a reduction in the aircraft weight and block fuel penalties incurred with low fan pressure ratio, ultra-high bypass ratio designs. This enables lower noise levels to be pursued (through lower fan pressure ratio) with minor negative impacts on aircraft weight and fuel efficiency. Regardless of the engine design selected, the results of this study indicate the potential for the advanced aircraft to realize substantial improvements in fuel efficiency, emissions, and noise compared to the current engines in this size class https://jeasd.uomustansiriyah.edu.iq/index.php/jeasd/article/view/1097turbofan enginesbypass rationoise reductionspecific thrustSpecific fuel consumption |
| spellingShingle | Marwan Fakhri Basher Optimum Turbofan Engine Performance Through Variation of Bypass Ratio Journal of Engineering and Sustainable Development turbofan engines bypass ratio noise reduction specific thrust Specific fuel consumption |
| title | Optimum Turbofan Engine Performance Through Variation of Bypass Ratio |
| title_full | Optimum Turbofan Engine Performance Through Variation of Bypass Ratio |
| title_fullStr | Optimum Turbofan Engine Performance Through Variation of Bypass Ratio |
| title_full_unstemmed | Optimum Turbofan Engine Performance Through Variation of Bypass Ratio |
| title_short | Optimum Turbofan Engine Performance Through Variation of Bypass Ratio |
| title_sort | optimum turbofan engine performance through variation of bypass ratio |
| topic | turbofan engines bypass ratio noise reduction specific thrust Specific fuel consumption |
| url | https://jeasd.uomustansiriyah.edu.iq/index.php/jeasd/article/view/1097 |
| work_keys_str_mv | AT marwanfakhribasher optimumturbofanengineperformancethroughvariationofbypassratio |