ADAPTIVE RECTIFICATION OF PARAMETERS IN AEROENGINE SIMULATION MODEL

LQ/controller design for aero-engine based on improved NSGAⅡ

Mathematical model of isentropic expansion process based onfunction

Investigation on the performance of an ultrasonic/pressure-swirl hybrid injector

Chaos arithmetic for civil aero-engine forecasting

th Dept.Northwestern Polytechnical University

Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics

College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics

College of Aeronautical Engineering, Civil Aviation University of China

School of Power and Energy,Northwestern Polytechnical University