张帅 - 浙江大学 - 航空航天学院

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

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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