YÜKSEK BYPASSLI TURBOFAN MOTORLARININ TASARIM NOKTASI ANALİZLERİ
In this paper, on design analysis of high bypass turbofan engines with separate flow and no afterburning used in commercial aircraft was analysed and then effects of some design variables (e.g. compressor pressure ratio, fan pressure ratio ,turbine inlet temperature, bypass ratio, cooling air rati...
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Hezarfen Aeronautics and Space Technologies Institue
2008-01-01
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Series: | Havacılık ve Uzay Teknolojileri Dergisi |
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Online Access: | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/175/163 |
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doaj-c17ec86b5eba4f0487651d33c7916aff2020-11-24T21:31:47ZengHezarfen Aeronautics and Space Technologies InstitueHavacılık ve Uzay Teknolojileri Dergisi1304-04481304-04482008-01-013318YÜKSEK BYPASSLI TURBOFAN MOTORLARININ TASARIM NOKTASI ANALİZLERİÖnder Turan 0İlkay Orhan1T. Hikmet Karakoç2Anadolu UniversityAnadolu UniversityAnadolu UniversityIn this paper, on design analysis of high bypass turbofan engines with separate flow and no afterburning used in commercial aircraft was analysed and then effects of some design variables (e.g. compressor pressure ratio, fan pressure ratio ,turbine inlet temperature, bypass ratio, cooling air ratio, nozzles pressure losses) and effects of different flight conditions (e.g. flight altitude and flight Mach number) on the engine performance were investigated. A new software program had been developed for this purpose in Visual Basic 6.0 programming language. Values of the engine performance parameters such as specific fuel consumption and specific thrust were calculated and then performance curves were obtained in this software program.http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/175/163High Bypass TurbofanParametric AnalysisPreliminary DesignPropulsionGas Turbine |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Önder Turan İlkay Orhan T. Hikmet Karakoç |
spellingShingle |
Önder Turan İlkay Orhan T. Hikmet Karakoç YÜKSEK BYPASSLI TURBOFAN MOTORLARININ TASARIM NOKTASI ANALİZLERİ Havacılık ve Uzay Teknolojileri Dergisi High Bypass Turbofan Parametric Analysis Preliminary Design Propulsion Gas Turbine |
author_facet |
Önder Turan İlkay Orhan T. Hikmet Karakoç |
author_sort |
Önder Turan |
title |
YÜKSEK BYPASSLI TURBOFAN MOTORLARININ TASARIM NOKTASI ANALİZLERİ |
title_short |
YÜKSEK BYPASSLI TURBOFAN MOTORLARININ TASARIM NOKTASI ANALİZLERİ |
title_full |
YÜKSEK BYPASSLI TURBOFAN MOTORLARININ TASARIM NOKTASI ANALİZLERİ |
title_fullStr |
YÜKSEK BYPASSLI TURBOFAN MOTORLARININ TASARIM NOKTASI ANALİZLERİ |
title_full_unstemmed |
YÜKSEK BYPASSLI TURBOFAN MOTORLARININ TASARIM NOKTASI ANALİZLERİ |
title_sort |
yüksek bypassli turbofan motorlarinin tasarim noktasi anali̇zleri̇ |
publisher |
Hezarfen Aeronautics and Space Technologies Institue |
series |
Havacılık ve Uzay Teknolojileri Dergisi |
issn |
1304-0448 1304-0448 |
publishDate |
2008-01-01 |
description |
In this paper, on design analysis of high bypass turbofan engines with separate flow and no afterburning used in
commercial aircraft was analysed and then effects of some design variables (e.g. compressor pressure ratio, fan
pressure ratio ,turbine inlet temperature, bypass ratio, cooling air ratio, nozzles pressure losses) and effects of
different flight conditions (e.g. flight altitude and flight Mach number) on the engine performance were
investigated. A new software program had been developed for this purpose in Visual Basic 6.0 programming
language. Values of the engine performance parameters such as specific fuel consumption and specific thrust
were calculated and then performance curves were obtained in this software program. |
topic |
High Bypass Turbofan Parametric Analysis Preliminary Design Propulsion Gas Turbine |
url |
http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/175/163 |
work_keys_str_mv |
AT onderturan yuksekbypassliturbofanmotorlarinintasarimnoktasianalizleri AT ilkayorhan yuksekbypassliturbofanmotorlarinintasarimnoktasianalizleri AT thikmetkarakoc yuksekbypassliturbofanmotorlarinintasarimnoktasianalizleri |
_version_ |
1725959730158895104 |