Performance of a microjet using component map scaling

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) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 94 Sayı: 8
  • Basım Tarihi: 2022
  • Doi Numarası: 10.1108/aeat-02-2021-0056
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus, Academic Search Premier, ABI/INFORM, Aerospace Database, Compendex, INSPEC
  • Sayfa Sayıları: ss.1201-1219
  • Anahtar Kelimeler: Gas turbine engine, Off-design, On-design, Compressor map, Turbojet
  • 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.