Simulation-based steady-state aero-thermal model for small-scale turboprop engine
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.89, sa.2, ss.203-210, 2017 (SCI-Expanded, Scopus)
- 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
- Eskişehir Osmangazi 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.