INVESTIGATION OF LOW-PRESSURE TURBINE AND AIRCRAFT PERFORMANCE PARAMETERS THROUGH MULTIPLE REGRESSION ANALYSIS
Faults in aircraft performance can be identified by the experts via analysis of the recorded flight information in today`s aircraft technology. The parameters used in identification of the faults include exhaust gas temperature, fuel flow, engine fan speed, vibration, oil pressure and oil temperatur...
Main Author: | Mustagime Tülin YILDIRIM |
---|---|
Format: | Article |
Language: | English |
Published: |
Turkish Air Force Academy
2017-07-01
|
Series: | Havacılık ve Uzay Teknolojileri Dergisi |
Subjects: | |
Online Access: | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/8/8 |
Similar Items
-
Forced Response of a Low-Pressure Turbine Blade using Spectral/hp Element Method: Direct Numerical Simulation
by: Daniel H. Wacks, et al.
Published: (2021-01-01) -
Vibration Test of Blade Disc of High Pressure Turbine in High Rotating Speed
by: LUO Li, et al.
Published: (2021-02-01) -
Computational performance of a-100 kW low pressure turbine to recover gas turbine exhaust energy
by: A. A. Ahmad Zahidin
Published: (2019-06-01) -
Testing and Numerical Analysis of Abnormal Pressure Pulsations in Francis Turbines
by: Lu Jia, et al.
Published: (2024-01-01) -
INVESTIGATION OF THE EFFECT OF THE WAKE GENERATED BY ROTOR BLADES ON THE FLOW THROUGH STATOR PASSAGE FOR LOW PRESSURE TURBINE
by: Ihsan Y. Hussain, et al.
Published: (2010-06-01)