Simulation-based steady-state aero-thermal model for small-scale turboprop engine

YAZAR I., Yasa T., KIYAK E.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.89, sa.2, ss.203-210, 2017 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 89 Sayı: 2
  • Basım Tarihi: 2017
  • Doi Numarası: 10.1108/aeat-02-2015-0062
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.203-210
  • Anahtar Kelimeler: ANFIS, Compressor performance prediction, Nonlinear mathematical model, Turboprop engine, GAS-TURBINE ENGINE, GENETIC ALGORITHMS, MAP GENERATION, PERFORMANCE, PREDICTION, COMPRESSOR, ANFIS
  • Anadolu Üniversitesi Adresli: Evet

Özet

Purpose - An aircraft engine control system consists of a large scale of control parameters and variables because of the complex structure of aero-engine. Monitoring and adjusting control variables and parameters such as detecting, isolating and reconfiguring the system faults/failures depend on the controller design. Developing a robust controller is based on an accurate mathematical model.