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


YAZAR I. , Yasa T., KIYAK E.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.89, no.2, pp.203-210, 2017 (Journal Indexed in SCI) identifier identifier

  • Publication Type: Article / Article
  • Volume: 89 Issue: 2
  • Publication Date: 2017
  • Doi Number: 10.1108/aeat-02-2015-0062
  • Title of Journal : AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Page Numbers: pp.203-210

Abstract

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.