1988-2008, China Aerodynamic Research and Development Center, Research Fellow
2009-Now, Shanghai Jiao Tong University, Professor
1984-1988, Nanjing Aeronautic Institute, Bachelor
1989-1992, China Aerodynamics Development and Research Center, Master
1994-1997, Nanjing Aeronautic and Astronautic University, Doctor
Specialized in helicopter aerodynamic characteristics, dynamics and control, the mechanism of complex flow and control for aircraft, and the test techniques in wind tunnel.
(1) Advanced Airfoil and Blade Design for Rotorcraft, Pre-research
(2) The Flow Interference Mechanism between Rotors and Wings for Tilting Rotor Aircraft, Pre-research
(3) Aero-elastics Dynamics and Control for Helicopter Rotor, Pre-research
（1） Qiu Z , Wang F* . Aeroelastic responses of airfoil under dynamic stall forced to oscillate by cyclic pitch input[J]. Journal of Sound and Vibration, 2020:115366.
（2） Qiu Z, Xu W, Yuan J, and Wang F*. Secondary resonances in aeroelastic response of oscillating airfoil under dynamic stall[J]. Journal of Vibration and Control, 2018, 24(23): 5665-5680.
（3） Yuan J, Qi N, Qiu Z, Wang F*. Adaptive RBF observer-sliding mode controller design for a two dimensional aeroelastic system with unsteady aerodynamics[J]. Aerospace Science and Technology, 2018, 80: 482-495.
（4） Li G, Fu X, Wang F*. High-resolution multi-code implementation of unsteady Navier–Stokes flow solver based on paralleled overset adaptive mesh refinement and high-order low-dissipation hybrid schemes[J]. International Journal of Computational Fluid Dynamics, 2017, 31(9): 379-395.
（5） Li G, Fu X, Wang F*. High-order non-inertial computation method for helicopter rotor flows in forward flight[J]. International Journal of Numerical Methods for Heat & Fluid Flow, 2017, 27(12):2835-2857.
Honors and awards
A Second Prize of the National Science and Technology Progress Award, a First Prize and two Third Prizes in the Ministerial Science and Technology Progress Award.