ARDYANMALI VE AYRIK AKIŞLI TURBOFANLARDA FAN BASINÇ ORANI VE BYPASS ORANIYLA TOPLAM VERİMİN DEĞİŞİMİNİN İNCELENMESİ

Overall efficiency is an important design parameter of the engine in preliminary design and defined as the ratio of aircraft thrust power to the rate of thermal energy released in the engine. In this paper, effects of the fan pressure ratio and the bypass ratio on engine overall efficiency were in...

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Main Authors: Ömer Turan, T. Hikmet Karakoç
Format: Article
Language:English
Published: Turkish Air Force Academy 2009-07-01
Series:Havacılık ve Uzay Teknolojileri Dergisi
Subjects:
Online Access:http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/211/201
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author Ömer Turan
T. Hikmet Karakoç
author_facet Ömer Turan
T. Hikmet Karakoç
author_sort Ömer Turan
collection DOAJ
description Overall efficiency is an important design parameter of the engine in preliminary design and defined as the ratio of aircraft thrust power to the rate of thermal energy released in the engine. In this paper, effects of the fan pressure ratio and the bypass ratio on engine overall efficiency were investigated for afterburning and separate flow turbofans. With this purpose, fan pressure ratio⎯bypass ratio⎯overall efficiency three dimensional graphs were developed and then computer experiment results were evaluated for three different flight Mach number.
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spelling doaj.art-4fe27b6aa11e40f69973a00272e0cc002023-02-15T16:20:21ZengTurkish Air Force AcademyHavacılık ve Uzay Teknolojileri Dergisi1304-04481304-04482009-07-01426776ARDYANMALI VE AYRIK AKIŞLI TURBOFANLARDA FAN BASINÇ ORANI VE BYPASS ORANIYLA TOPLAM VERİMİN DEĞİŞİMİNİN İNCELENMESİÖmer Turan0T. Hikmet Karakoç1Anadolu UniversityAnadolu UniversityOverall efficiency is an important design parameter of the engine in preliminary design and defined as the ratio of aircraft thrust power to the rate of thermal energy released in the engine. In this paper, effects of the fan pressure ratio and the bypass ratio on engine overall efficiency were investigated for afterburning and separate flow turbofans. With this purpose, fan pressure ratio⎯bypass ratio⎯overall efficiency three dimensional graphs were developed and then computer experiment results were evaluated for three different flight Mach number.http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/211/201Separate flow turbofanAfterburnerOverall efficiencyAircraft propulsion
spellingShingle Ömer Turan
T. Hikmet Karakoç
ARDYANMALI VE AYRIK AKIŞLI TURBOFANLARDA FAN BASINÇ ORANI VE BYPASS ORANIYLA TOPLAM VERİMİN DEĞİŞİMİNİN İNCELENMESİ
Havacılık ve Uzay Teknolojileri Dergisi
Separate flow turbofan
Afterburner
Overall efficiency
Aircraft propulsion
title ARDYANMALI VE AYRIK AKIŞLI TURBOFANLARDA FAN BASINÇ ORANI VE BYPASS ORANIYLA TOPLAM VERİMİN DEĞİŞİMİNİN İNCELENMESİ
title_full ARDYANMALI VE AYRIK AKIŞLI TURBOFANLARDA FAN BASINÇ ORANI VE BYPASS ORANIYLA TOPLAM VERİMİN DEĞİŞİMİNİN İNCELENMESİ
title_fullStr ARDYANMALI VE AYRIK AKIŞLI TURBOFANLARDA FAN BASINÇ ORANI VE BYPASS ORANIYLA TOPLAM VERİMİN DEĞİŞİMİNİN İNCELENMESİ
title_full_unstemmed ARDYANMALI VE AYRIK AKIŞLI TURBOFANLARDA FAN BASINÇ ORANI VE BYPASS ORANIYLA TOPLAM VERİMİN DEĞİŞİMİNİN İNCELENMESİ
title_short ARDYANMALI VE AYRIK AKIŞLI TURBOFANLARDA FAN BASINÇ ORANI VE BYPASS ORANIYLA TOPLAM VERİMİN DEĞİŞİMİNİN İNCELENMESİ
title_sort ardyanmali ve ayrik akisli turbofanlarda fan basinc orani ve bypass oraniyla toplam verimin degisiminin incelenmesi
topic Separate flow turbofan
Afterburner
Overall efficiency
Aircraft propulsion
url http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/211/201
work_keys_str_mv AT omerturan ardyanmaliveayrikakisliturbofanlardafanbasincoranivebypassoraniylatoplamverimindegisimininincelenmesi
AT thikmetkarakoc ardyanmaliveayrikakisliturbofanlardafanbasincoranivebypassoraniylatoplamverimindegisimininincelenmesi