Design optimization of a mixed-flow compressor impeller for a small turbojet engine

Cevik M., UZOL O.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.83, sa.3, ss.127-137, 2011 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 83 Sayı: 3
  • Basım Tarihi: 2011
  • Doi Numarası: 10.1108/00022661111131212
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.127-137
  • Anahtar Kelimeler: Jet engines, Optimum design, Compressors
  • Orta Doğu Teknik Üniversitesi Adresli: Evet

Özet

Purpose - This paper aims to present the results of a design optimization study for the impeller of a small mixed-flow compressor. The objective of the optimization is to obtain an impeller geometry that could minimize a cost function based on the specific thrust and the thrust specific fuel consumption of a small turbojet engine.