Control strategy of active magnetic bearing system based on variable bias current control

Experimental study of static-thrust propeller for mini-vertical takeoff and landing (VTOL) aircraft

VALIDATION TESTS WITH A SCALE-MODEL FOR SURFACE SOUND PRESSURE PREDICTION OF PROPELLER AIRCRAFT

EXPERIMENTAL STUDY ON GASDYNAMIC PERFORMANCE OF INTAKE WITH PLENUM BYPASS

EXPERIMENTAL STUDY ON PROPELLER FENCE FOR EFFICIENCY ENHANCEMENT AND NOISE REDUCTION

Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology, College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics

Department of Design Engineering, Nanjing University of Aeronautics and Astronautics

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

th Dept.Beijing University of Aeronautics and Astronautics

nd Dept.,Nanjing University of Aeronautics and Astronautics