2011-06~现在, 力学研究所, 副研究员
2009-04~2011-06,新加坡国立大学, Research Scientist
2009-01~2009-04,庆尚国立大学(韩国), Academic Research Professor
2006-03~2008-12,庆尚国立大学(韩国), Senior Researcher
2000-09~2006-01,中科院力学研究所, 博士
1994-07~2000-07,青岛捷能汽轮机股份公司, 助理工程师
1990-09~1994-07,大连理工大学动力工程系, 学士
社会兼职
2016-04-20-今,激波与激波管专业委员会, 委员
教授课程
气体动力学基础
计算流体力学初步
专利与奖励
奖励信息
(1) 复现高超声速飞行条件激波风洞研究集体, 部委级, 2016
专利成果
出版信息
发表论文
(1) A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections, Aerospace Science and Technology, 2019-12, 第 3 作者
(2) Weighting by cross-validation: A calibration method for force measurements via transient response analysis, Experimental Techniques, 2019-09, 第 3 作者
(3) Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures, Aerospace Science and Technology, 2019-07, 第 3 作者
(4) 旋转爆轰波中多波流动模式的数值研究, 推进技术, 2019-02, 第 4 作者
(5) Spectralmeasurements of hypervelocity flow in an expansion tunnel, Acta Mechanica Sinica, 2019-01, 第 4 作者
(6) Numerical investigation of oblique detonations induced by a finite wedge in a stoichiometric hydrogen-air mixture, Fuel, 2018, 第 2 作者
(7) Numerical investigation of the effects of shock tube geometry on the propagation of an ideal blast wave profile, Shock Waves, 2017, 第 2 作者
(8) Shock relations in gases of heterogeneous thermodynamic properties, Science China Technology Sciences, 2017, 第 1 作者
(9) 振动激发对激波反射的影响, 航空学报, 2017, 第 4 作者
(10) JF-16膨胀管流场分析及升级改造, 航空学报, 2016, 第 3 作者
(11) Starting Process in a Large-Scale Shock Tunnel, AIAA Journal, 2016, 第 2 作者
(12) Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity, Sci China Tech Sci, 2016, 第 2 作者
(13) 可压缩流体粘性系数的连续介质理论, 中国科学:物理学力学天文学, 2016, 第 2 作者
(14) 爆轰驱动膨胀管性能研究, 航空学报, 2016, 第 3 作者
(15) On the numerical technique for the simulation of hypervelocity test flows, Comput. Fluids, 2015, 第 1 作者
(16) 一种基于AUSM思想的通量分裂方法, 计算物理, 2015, 第 2 作者
(17) 高超声速流动上仰异常现象关键因素数值研究, 中国科学:物理学 力学 天文学, 2015, 第 2 作者
(18) 热化学非平衡流动中黏性干扰和化学反应对HB2气动力的影响, 中国科学:物理学 力学 天文学, 2015, 第 2 作者
(19) 高焓热化学非平衡流动中再压缩效应对球锥气动力的影响, 力学学报, 2015, 第 2 作者
(20) Development of the detonation-driven expansion tube for orbital speed experiments, Science China Technology Sciences, 2015, 第 4 作者
(21) Relative contribution ratio: A quantitative metrics for multi-parameter analysis, Cogent Mathematics, 2015, 第 2 作者
(22) Thermo-chemical nonequilibrium phenomena of the strong shock wave to generate hypervelocity test flow, International Journal of Modern Physics, 2014, 第 1 作者
(23) Numerical simulation of deflagration to detonation transition in a straight duct: Effects of energy release and detonation stability, Advances in Applied Mathematics and Mechanics, 2014, 第 2 作者
(24) The simulation of unsteady cavitating flows with external perturbations, Comput. Fluids, 2013, 第 1 作者
(25) Numerical predictions for the hypervelocity test flow conditions of JF-16, The 29th International Symposium on Shock Waves, 2013, 第 1 作者
(26) Simulation of wave-flow-cavitation interaction using a compressbile homogenous flow method, Commun. Comput. Phys., 2012, 第 3 作者
(27) 激波反射现象的研究进展, 力学进展, 2012, 第 3 作者
(28) 激波与爆轰波对撞的二维数值模拟, 力学学报, 2012, 第 3 作者
(29) On the modified dispersion-controlled-dissipative (DCD) scheme for computation of flow supercavitation, Computers and Fluids, 2011, 第 1 作者
(30) Reconsideration of inviscid shock interactions and transition phenomena on double-wedge geometries in a Ma=9 hypersonic flow, Theoretical and Computational Fluid Dynamics, 2011, 第 1 作者
(31) Geometric criterion for RR-MR transition in hypersonic double-wedge flows, Physics of Fluids, 2010, 第 1 作者
(32) Computational confirmation of an abnormal Mach reflection configuration, Physics of Fluids, 2009, 第 1 作者
(33) Downstream flow condition effects on the RR-MR transition of asymmetric shock waves in steady flows, Journal of Fluid Mechanics, 2009, 第 1 作者
(1)Hypersonic Flow Conditions for Aerodynamic Tests of a Martian Entry Model in the Shock Tunnel JF12 2019-07-13
(2)Computer-aid diagnostic of hypersonic test flow in a shock-expansion tube Hu ZM, Jiang ZL 2013-08-25
(3)Numerical predictions for the hypervelocity test flow conditions of JF-16 Hu ZM, Jiang ZL 2013-07-14
(4)Thermo-chemical nonequilibrium phenomena of the strong shock wave to generate hypervelocity test flow Hu ZM, Wang C, Jiang ZL 2013-06-09
(5)Analysis of the test condition of a shock-expansion tube Hu ZM, Wu B, Jiang ZL 2012-10-15
(6)Vortex Generation Arising from the interaction of shock wave and fuel bubble Hu Zm, Jiang ZL, Dou HS 2012-07-04
(7)CFD for chemically reacting flow and its applications Hu ZM, Sun XF, Jiang ZL 2012-05-30
(8) Reconsideration RR-MR transition in steady flows: Symmetric vs. asymmetric reflection Z.M. Hu, M.S. Kim, R.S. Myong, T.H Cho 2008-07-15
(9)Numerical study of shock interactions in viscous, hypersonic flows over double-wedge geometries Z.M. Hu, R.S. Myong, T.H Cho 2007-07-15