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个人简介

1977年12月26日生。1996年进入西安交通大学能源与动力工程学院,2000年获热能与动力工程专业学士学位,2003年获动力工程及工程热物理专业硕士学位。同年去日本九州大学工学部,2006年获工学博士学位,2006年10月至2009年3月任学术研究员。2009年3月加盟浙江大学航空航天学院飞行器设计研究所。 教学工作 1,《热力学基础》 2,《航空航天概论》 3,《传热传质分析》 教学与课程 本科生《热力学基础》 本科生《航空航天概论》 研究生《传热传质分析》 科研 1,高超声速飞行器机体推进一体化设计与优化 2,无网格法 学术活动 Gou Wen-jin,Zhang Shuai,Zheng Yao.Implementation of the Moving Particle Semi-implicit Method for Free-Surface Flows on GPU Clusters,International Symposium on Computational Mechanics 2018,Aug.19-23,2018.

研究领域

计算流体力学及数值传热学 高超声速飞行器机体推进一体化设计与优化 无网格法

近期论文

查看导师新发文章 (温馨提示:请注意重名现象,建议点开原文通过作者单位确认)

Design and Verification of Minimum Length Nozzles with Specific/Variable Heat Ratio Based on Method of Characteristics,,13,6:- Back pressure characteristics of jaws inlet with constant-area isolator,,50,7:1418-1424 Simulation of isothermal multi-phase fuel-coolant interaction using MPS method with GPU acceleration,,81,3:330-336 A New High-Order Compact Scheme of Unstructured Finite Volume Method,,13,5:- Performances analysis of asymmetric minimum length nozzles,,7,2:- Experimental investigation of a single trapped-vortex combustor with a slight temperature raise,,14,7:520-525 Experimental investigation of a single trapped-vortex combustor with a slight temperature raise,,14,7:520-525 A preliminary study on empirical correlation of lean blow-out based on trapped vortex combustor,,31,10:1914-1918 A feature-based data mining method for fluid dynamics,,28,5:540-546 Modified PSO method for automating transfer function designing in volume rendering,,44,8:1466-1472 Simulation of surface tension force using moving particle semi-implicit method,,28,3:345-349 Experimental and numerical study on temperature variation and air flow distribution in trapped votex combustor,,32,2:182-187 Experiment and simulation study on lean blow-out of trapped vortex combustor with various aspect ratios,,18,1:48-55 An optimal study on a TVC evaporation tube using moving particle semi-implicit method,,32,3:339-342 Experiment and simulation study on lean blow-out of trapped vortex combustor with various aspect ratios,,18,1:48-55 Numerical simulation of the transient shape of the red blood cell in microcapillary flow,,36,:174-183 Surrogate models characteristic analysis and optimization for waverider aerodynamic design,,38,4:451-457

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