
CHENG Yongsheng
Senior Laboratory Technician
School of Aeronautics and Astronautics, Room A324
yscheng@sjtu.edu.cn
Educational Background
- 1992 - 1996, Shanghai Jiao Tong University, Bachelor
- 1999 - 2002, Shanghai Jiao Tong University, Master
- 2001 - 2006, Shanghai Jiao Tong University, Doctor
Work Experience
- 2006-2009,Shanghai Jiao Tong University,Post Doctor
- 2009-2016,Shanghai Jiao Tong University,Lecturer
- 2017-Present,Shanghai Jiao Tong University,Senior Laboratory Technician
Research Interests
- Aircraft Design
- Unsteady Aerodynamics
- Computational Fluid Dynamics
- Airworthiness Management
- Flight Test
Representative Papers And Monographs
- FuZhidong, ChengYongsheng, Liu Hong. Numerical Investigation of a NACA 0012Airfoil inOscillatory Motions, Journalof Aircraft,49(6), 2012.
- Fu X,Wu J.C., Cheng Y.S.An improved method solving the Neumann Problem and itsapplication incalculating the apparent mass coefficient for incompressibleaxisymmetricpotential flow. The 2nd International Retreat on Vortex Dynamicsand VorticityAerodynamics,August, 2013.
- ChengYongsheng,DengKangyao , Li Tao. The coupling influence of airflow andtemperature on thewall-wetted fuel film distribution. Experimental Thermal andFluid Science.2010,34(2):227-233.
- ChengYongsheng,DengKangyao , Li Tao. Measurement and simulation of wall-wettedfuel film thickness.International Journal of Thermal Sciences. 2010,49(4):733-739.
- Cheng Yongsheng,Liu Hua, Deng Kangyao. Numerical Simulation of the Fluid Flowsarounda Missile with Thrust-vectoring Control System Launched Underwater. Journal of Ship Mechanics, 2008, 12(6):845-857.
- ChengYongsheng, LiuHua. A Coupling Model of Water Flows and Gas Flows in Exhausted Gas Bubble on Missile Launched Under water.Journal of Hydrodynamics, 2007,Ser.B,19(4):403-411. ChengYongsheng,LiuHua.MathematicalModelingofFluidFlowsforUnderwaterMissileLaunch. JournalofHydrodynamics,2006, v 18, n 3SUPPL., July,492-497.