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


Cevik M., UZOL O.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.83, ss.127-137, 2011 (SCI İndekslerine Giren Dergi) identifier identifier

  • Cilt numarası: 83 Konu: 3
  • Basım Tarihi: 2011
  • Doi Numarası: 10.1108/00022661111131212
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Sayfa Sayıları: ss.127-137

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.