程用胜

（1）FuZhidong, ChengYongsheng, Liu Hong. Numerical Investigation of a NACA 0012Airfoil inOscillatory Motions, Journalof Aircraft,49(6), 2012.

（2）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，2013年8月。

（3）马明，程用胜。基于涡量场的二维物体非定常气动力计算。微型电脑应用，2013,29(4):47-49。

（4）韩龙,陈阳陵,王福新,程用胜.高海况机翼波浪地面效应数值模拟与分析.上海交通大学学报,2014,48(8),1127-1133.

（5）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.

（6）ChengYongsheng,DengKangyao , Li Tao. Measurement and simulation of wall-wettedfuel film thickness.International Journal of Thermal Sciences. 2010,49(4):733-739.

（7）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.

（8）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.

（9）ChengYongsheng,LiuHua.MathematicalModelingofFluidFlowsforUnderwaterMissileLaunch. JournalofHydrodynamics,2006, v 18, n 3SUPPL., July,492-497.

（10）程用胜, 邓康耀, 李韬. 喷嘴距离和喷嘴角度对油膜附壁的影响. 燃烧科学与技术, 2009,15(2):167-171.

（11）程用胜, 陆振华, 邓康耀等.空气流速对附壁油膜分布影响的实验研究. 内燃机学报, 2008,26(5):429-433.

（12）程用胜，刘桦.　喷管不同摆角对水下发射导弹受力的影响.　水动力学研究与进展,2007,Ser.A,22(1):83-92.

（13）程用胜，刘桦，薛雷平.　采用NND方法计算三维喷管气流场.　力学季刊,2005,26(4):529-533.