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Dep. of Aircratft Design

Cheng Yongsheng

 

 

Yongsheng Cheng

Senior Engineer

Tel: 021-34208602

Email: yscheng@sjtu.edu.cn

Office: 1312, School of Aeronautics and Astronautics Building

 

Work Experience

2016.12-present: School of Aeronautics and Astronautics, Shanghai Jiao Tong University,Senior Engineer

2009.07-2016.11: School of Aeronautics and Astronautics, Shanghai Jiao Tong University,Assistant Professor

2006.09-2009.03: School of Mechanical Engineering, Shanghai Jiao Tong University,Postdoctor

Education

2001.09-2006.08: Department of Engineering Mechanics, Shanghai Jiao Tong University, Ph.D.

1999.09-2002.03: Department of Engineering Mechanics, Shanghai Jiao Tong University, Master

1992.09-1996.07: Department of Mechanical Engineering, Shanghai Jiao Tong University, Bachelor

Research Field

Aircraft Design, Unsteady Aerodynamics, Computational Fluid Dynamics

Main research projects

  1. Equivalent Level of Safety for Out-of-trim Research, 2016-2020
  2. Maneuvering Speed Limit Special Condition Research, 2016-2020
  3. Random Waves Physical Characteristics Description Method Research, 2017
  4. Research on the prediction method of the trajectory of the shedding fan ice from the aircraft engine, 2015-2016

Publications

  1. Fu Zhidong, Cheng Yongsheng, Liu Hong. Numerical Investigation of a NACA 0012 Airfoil in Oscillatory Motions,  Journal of Aircraft, 49(6):2095-2099, 2012.
  2. Fu X, Wu J.C., Cheng Y.S. An improved method solving the Neumann Problem and its application in calculating the apparent mass coefficient for incompressible axisymmetric potential flow. The 2nd International Retreat on Vortex Dynamics and Vorticity Aerodynamics,August, 2013.
  3. Cheng Yong-sheng, Deng Kangyao , Li Tao. The coupling influence of airflow and temperature on the wall-wetted fuel film distribution. Experimental Thermal and Fluid Science. 2010,34(2):227-233. 
  4. Cheng Yong-sheng, Deng Kangyao , Li Tao. Measurement and simulation of wall-wetted fuel film thickness. International Journal of Thermal Sciences. 2010,49(4):733-739.   
  5. Cheng  Yong-sheng,  Liu  Hua,  Deng  Kangyao.  Numerical Simulation of the Fluid Flows around a Missile with Thrust-vectoring Control System Launched Underwater.  Journal of  Ship Mechanics, 2008, 12(6):845-857.  
  6. Cheng Yong-sheng, Liu Hua. A Coupling Model of Water Flows and Gas Flows in Exhausted Gas Bubble on Missile Launched Underwater. Journal of Hydrodynamics, 2007, Ser. B, 19(4): 403-411.
  7. Cheng Yong-sheng, Liu Hua. Mathematical Modeling of Fluid Flows for Underwater Missile Launch.  Journal of Hydrodynamics, 2006, v 18, n 3 SUPPL., July, 492-497.

 

 

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Technical Support: WeiCheng

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