RELATIONSHIP BETWEEN BLADE FLUTTER AND LEAKAGE VORTEX OF COMPRESSOR ROTOR

Incipient fault detection for aero-engine rotor based on frequency compression of stochastic resonance

Faults analysis and solution in ground operation of a micro turbojet engine

AEROELASTIC OPTIMIZATION OF A HELICOPTER ROTOR WITH SINGLE-CELL COMPOSITE BLADES FOR VIBRATION REDUCTION

PREDICTION FOR NONLINEAR PERIODIC SOLUTIONS OF UNBALANCED ROTOR BEARING SYSTEM

th Dept.Beijing University of Aeronautics and Astronautics

Xi'an Institute Optics and Precision Mechanics, Chinese Academy of Sciences

School of Information and Communication Engineering, Guilin University of Electronic Technology

School of Transportation Science and Engineering,Beijing University of Aeronautics and Astronautics

School of Astronautics, Beijing University of Aeronautics and Astronautics