Atıf İçin Kopyala
Coban K., Ekici S., ÇOLPAN C. Ö., Karakoc T. H.
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.94, sa.8, ss.1201-1219, 2022 (SCI-Expanded)
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Yayın Türü:
Makale / Tam Makale
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Cilt numarası:
94
Sayı:
8
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Basım Tarihi:
2022
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Doi Numarası:
10.1108/aeat-02-2021-0056
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Dergi Adı:
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
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Derginin Tarandığı İndeksler:
Science Citation Index Expanded (SCI-EXPANDED), Scopus, Academic Search Premier, ABI/INFORM, Aerospace Database, Compendex, INSPEC
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Sayfa Sayıları:
ss.1201-1219
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Anahtar Kelimeler:
Gas turbine engine, Off-design, On-design, Compressor map, Turbojet
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Dokuz Eylül Üniversitesi Adresli:
Evet
Özet
Purpose - This paper aims to investigate the cycle performance of a small size turbojet engine used in unmanned aerial vehicles at 0-5,000 m altitude and 0-0.8 Mach flight speeds with real component maps.