中国·3044AM永利集团(股份)有限公司-官方网站

Faculty
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.
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