Robust fault diagnosis for aero-engine compressor sensor based on LMI and discrete model
Effect of inlet wake angle on compressor stator loading
Influence of turbulence models on simulation of a compressor
Numerical simulation of the effect of blade tip blowing on a low speed axial compressor tip clearance flow
Fracture Analysis of the 2nd Stage Compressor Blade in an Aeroengine
Related Author
HE Chen
ZHANG Xiao-dong
Patton R J
YANG Rong-fei
LI Qiu-shi
LI Zhi-ping
ZHOU Sheng
YIN Song
Related Institution
Control and Intelligent Systems Engineering,Faculty of Science,University of Hull,Hull HU6 7RX,United Kingdom
School of Power and Energy,Northwestern Polytechnical University
National Key Laboratory of Science and Technology on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Key Laboratory of Condition Monitoring and Control for Power Plant Equipment, Ministry of Education,Department of Power,School of Energy and Power Engineering, North China Electric Power University