On-design exergy analysis of a combustor for a turbojet engine: a parametric study

Topal A., TURAN Ö.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.89, sa.5, ss.719-724, 2017 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 89 Sayı: 5
  • Basım Tarihi: 2017
  • Doi Numarası: 10.1108/aeat-12-2016-0254
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.719-724
  • Anahtar Kelimeler: Exergy, Gas turbine, Propulsion, Combustor, Turbojet, BYPASS TURBOFAN ENGINE, TURBINE POWER-PLANTS, TURBOPROP ENGINE, GENERATION, EFFICIENCY, ALGORITHM, ENERGY, AID
  • Anadolu Üniversitesi Adresli: Evet

Özet

Purpose - The purpose of this study is to perform an exergy analysis of a turbojet engine combustor at different cycle parameters. Design/methodology/approach - Base cycle parameters have been defined for the engine, and then differentiation of the combustor exergy efficiencies and destruction rates have been evaluated by changing overall pressure ratio, combustor exit temperature and combustor pressure ratio.