Performance of a microjet using component map scaling

Coban K., Ekici S., ÇOLPAN C. Ö., Karakoc T. H.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.94, no.8, pp.1201-1219, 2022 (SCI-Expanded) identifier identifier

  • Publication Type: Article / Article
  • Volume: 94 Issue: 8
  • Publication Date: 2022
  • Doi Number: 10.1108/aeat-02-2021-0056
  • Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus, Academic Search Premier, ABI/INFORM, Aerospace Database, Compendex, INSPEC
  • Page Numbers: pp.1201-1219
  • Keywords: Gas turbine engine, Off-design, On-design, Compressor map, Turbojet
  • Dokuz Eylül University Affiliated: Yes

Abstract

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.