职称:教授

电话:+86 10 6277 2917

E-mail address:zhanghq@tsinghua.edu.cn

个人简介

张会强,清华大学航天航空学院教授,博士生导师

教育背景

1997.12 清华大学工程力学系工学博士

1991.05 航天部11所工学硕士

1988.07 国防科技大学航天技术系工学学士

工作履历

2011.12 - 清华大学航天航空学院推进与动力工程研究所,教授

2006.03 - 2007.03 美国普林斯顿大学机械与航空工程系,访问学者

2000.08 - 2011.12 清华大学工程力学系/航天航空学院,副教授

1998.01 - 2000.08 清华大学工程力学系工程热物理研究所,讲师

1991.05 - 1993.1 航天部十一所,助理工程师

课程教学

1、 《推进原理与技术》,本科生课程

2、 《发动机结构与系统设计》,本科生课程

3、 《火箭发动机》,本科生课程

4、 《燃烧过程的化学动力学分析》,本科生课程

5、 《飞行器基础实验》,本科生课程

6、 《航空航天导论》,本科生课程

7、《高等推进测试技术与实验》,研究生课程

8、《计算传热学》,研究生课程

研究领域

1. 燃烧不稳定性

2. 液体射流/液膜破碎雾化

3. 湍流两相反应流模型与细观模拟

4. 航空宇航发动机燃烧

5. 组合动力

研究概况

燃烧不稳定性:提出燃烧不稳定性的局部准定容燃烧激发机制,并定义了第三邓克尔来表征局部准定容燃烧。在汽油机、火箭发动机、燃气涡轮发动机和冲压发动机等动力型式中证实了该激发方式,而不同动力型式中的差异仅仅体现在局部准定容燃烧的形成机制各有不同,如:末端自燃、临界蒸发、粉尘爆炸、火上浇油、涡瓣压缩及二次破碎等。针对液体火箭发动机液-液撞击式雾化燃烧过程揭示了燃烧不稳定性的休伊特准则的物理机制,并提出了超级休伊特准则。

液体射流/液膜破碎雾化:揭示了液氧/煤油火箭发动机气液同轴喷嘴环形煤油液膜的雾化破碎机理以及旋流的抗脱壁效应而非雾化效应;揭示了燃气涡轮发动机煤油旋流液膜冲击破碎雾化和扩展破碎雾化两种模式,使得宽工况范围雾化特性具有一致性;揭示了氢氧气液同轴喷嘴中心液氧射流端面触发、横向流动-凹坑相互激发的破碎雾化新机制。

湍流两相反应流模型与细观模拟:发展了一系列湍流两相流动与燃烧模型,自主开发了有限反应速率框架下的湍流两相流动与燃烧过程的细观数值模拟平台,为机理研究和工程应用奠定了基础。

航空宇航发动机燃烧:提出了火箭发动机气液同轴喷嘴设计方法;建立了喷注面板喷嘴最小间距准则;提出了带缩进气液同轴喷嘴燃烧室稳定燃烧的三重机制:缩进区着火与火焰锚定、主燃区扩散火焰形态和单喷注单元燃烧流管化。

组合动力:提出了DRBCC组合动力概念;揭示了全速域飞行中不同动力模态对飞行特性的影响规律,冲压模态推力陷阱是提高其入轨飞行特性的瓶颈。

奖励与荣誉

1、 2002年北京市科学技术奖三等奖

2、 2020年北京市科学技术奖二等奖

3、 2022年某省部级科学技术进步奖二等奖

4、 2020年中国发明协会发明创新奖

5、 2021年中国发明协会发明创新奖

6、 2018、2022清华大学年度教学优秀奖

学术兼职

1、中国空气动力学会燃烧空气专业组副主任委员

2、《固体火箭技术》第八届编委会副主任委员

3、《火箭推进》第十一届编委会委员

4、航天液体动力全国重点实验室学术委员会委员

学术成果

[1]Leqi Lyu, Xin Jin and Huiqiang Zhang, Numerical investigation on the atomization process in a hydrogen-oxygen gas-liquid coaxial injector, Aerospace Science and Technology, 174, July 2026

[2]Li TQ, Zhang HQ and Wang B, Stability analysis of premixed flames with downstream heat gain, AEROSPACE SCIENCE AND TECHNOLOGY, 151, AUG 2024

[3]Liu Y, Liu G, Xu H, Chen L, Qin S, Chao Y and Zhang HQ, Research on breakup length and atomization characteristics of the swirl liquid sheet in perforation disintegration mode, PHYSICS OF FLUIDS, 35(12), DEC 2023

[4]Fei SB, Qi YL, Liu W, Wang YD, Wang Z and Zhang HQ, Combustion Modes Induced by Oil-Droplet Gas-Phase Pre-ignition in the Chamber under Different Environmental Conditions, COMBUSTION SCIENCE AND TECHNOLOGY, 195(2):379-397, JAN 25 2023

[5]Liu Y, Zhang Q, Zhang HQ and Wang B, Numerical investigation on the performance of internal flow and atomization in the recessed gas-centered swirl coaxial injectors, AEROSPACE SCIENCE AND TECHNOLOGY, 129, OCT 2022

[6]Song ZG, Zhao CJ, Zhang HQ, Dong T, Ma AJ, Yan DW, Research on Aircraft Attitude Control Method Based on Linear Active Disturbance Rejection, INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2022, AUG 17 2022

[7]Ji ZF, Zhang B, Zhang HQ, Wang B and Wang C, Reduction of feedback pressure perturbation for rotating detonation combustors, AEROSPACE SCIENCE AND TECHNOLOGY, 126, JUL 2022

[8]Liu Y, Zhang HQ, Li YF and Zhao ZJ, Numerical investigation on the hole characteristics and perforation mechanism of conical liquid sheet, THERMAL SCIENCE AND ENGINEERING PROGRESS, 29, MAR 1 2022

[9]Ji ZF, Zhang HQ and Wang B, Thermodynamic performance analysis of the rotating detonative airbreathing combined cycle engine,AEROSPACE SCIENCE AND TECHNOLOGY, 113, JUN 2021

[10]Chen Q and Zhang HQ, A compatible inlet condition for simulation of supersonic reacting mixing layers, AEROSPACE SCIENCE AND TECHNOLOGY, 111, APR 2021

[11]Qin JX, Zhou LX, Zhang HQ and Wang B, Numerical evaluation of acoustic characteristics of a thrust chamber with quarter-wave resonators, SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 64(2):375-386, FEB 2021

[12]Cui G and Zhang HQ, Hardware-in-the-loop simulation of flight mach fuzzy controller, WIRELESS NETWORKS, 27(5):3655-3663(SI), JUL 2021

[13]Gao DK, Qin JX and Zhang HQ, Investigation on Acoustic Properties of Thruster Chamber with Coaxial Injectors and Plenum Chamber, INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2020, SEP 25 2020

[14]Qin JX and Zhang HQ, Numerical Analysis of Self-Excited Combustion Instabilities in a Small MMH/NTO Liquid Rocket Engine, INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2020, JUL 4 2020

[15]Ji ZF, Duan RZ, Zhang RS, Zhang HQ and Wang B, Comprehensive Performance Analysis for the Rotating Detonation-Based Turboshaft Engine, INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2020, JUL 2 2020

[16]Ji ZF, Zhang HQ, Wang B and He W, Comprehensive Performance Analysis of the Turbofan With a Multi-Annular Rotating Detonation Duct Burner, JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 142(2), FEB 1 2020

[17]Fei SB, Wang Z, Qi YL, Wang YD and Zhang HQ, Ignition of a Single Lubricating Oil Droplet in Combustible Ambient Gaseous Mixture under High-Temperature and High-Pressure Conditions, COMBUSTION SCIENCE AND TECHNOLOGY, 191(11):2033-2052, NOV 2 2019

[18]Ji ZF, Zhang HQ and Wang B, Thrust control strategy based on the minimum combustor inlet Mach number to enhance the overall performance of a scramjet engine, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 233(13):4810-4824, OCT 2019

[19]Ji ZF, Zhang HQ and Wang B, Performance analysis of dual-duct rotating detonation aero-turbine engine, AEROSPACE SCIENCE AND TECHNOLOGY, 92:806-819, SEP 2019

[20]Guo HJ, Li YF, Xu HM, Shuai SJ and Zhang HQ, Interaction between under-expanded flashing jets: A numerical study, INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 137:990-1000, JUL 2019

[21]Wang WL and Zhang HQ, Laminar burning velocities of C2H4/N2O flames: Experimental study and its chemical kinetics mechanism, COMBUSTION AND FLAME, 202:362-375, APR 2019

[22]Guo HJ, Li YF, Wang B, Zhang HQ and Xu HM, Numerical investigation on flashing jet behaviors of single-hole GDI injector, INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 130:50-59, MAR 2019

[23]Li TQ, Zhang HQ and Yang F, Limit map of pulsating instability in hydrogen/air partially premixed counterflow flames, COMBUSTION AND FLAME, 201:170-180, MAR 2019

[24]Zhang F, Zhang HQ and Wang B, Conceptual study of a dual-rocket-based-combined-cycle powered two-stage-to-orbit launch vehicle, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 232(5):944-957, APR 2018

[25]Qin JX, Zhang HQ and Wang B, Numerical evaluation of acoustic characteristics and their damping of a thrust chamber using a constant-volume bomb model, CHINESE JOURNAL OF AERONAUTICS, 31(3):470-480, MAR 2018

[26]Lu H, Zhao WJ, Zhang HQ, Wang B and Wang XL, Particle transport behavior in air channel flow with multi-group Lagrangian tracking,CHINESE PHYSICS B, 26(1), JAN 2017

[27]Lu H, Zhao WJ, Zhang HQ, Wang B and Wang XL, Three-dimensional turbulent flow over cube-obstacles, CHINESE PHYSICS B, 26(1), JAN 2017

[28]Qian C, Bing W, Zhang HQ, Zhang YL and Wei, G, Numerical investigation of H2/air combustion instability driven by large scale vortex in supersonic mixing layers, INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 41(4):3171-3184, JAN 30 2016

[29]Wang B, Wei W, Zhang YL, Zhang HQ and Xue SY, Passive scalar mixing in Mc<1 planar shear layer flows, COMPUTERS & FLUIDS, 123:32-43, DEC 21 2015

[30]Wang B, Ren ZX and Zhang HQ, Stochastic separated flow models with applications in numerical computations of supersonic particle-laden turbulent flows, ADVANCES IN MECHANICAL ENGINEERING, 7(8), AUG 2015

[31]Qi YL, He X, Wang Z, Wang JX, Zhang HQ and Jiang YZ, An experimental investigation of super knock combustion mode using a one-dimensional constant volume bomb, INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 40(5):2377-2385, FEB 9 2015

[32]Zhang YL, Wang B, Zhang HQ and Xue SY, Mixing Enhancement of Compressible Planar Mixing Layer Impinged by Oblique Shock Waves, JOURNAL OF PROPULSION AND POWER, 31(1):156-169, JAN-FEB 2015

[33]Zhang YL, Wang B and Zhang HQ, Ignition, flame propagation and extinction in the supersonic mixing layer flow, SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 57(11): 2256-2264, NOV 2014

[34]Yang F, Zhang HQ, Chen Z and Kong WJ, Interaction of pressure wave and propagating flame during knock, INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 38(35): 15510-15519, NOV 22 2013

[35]Lu H, Wang B and Zhang HQ, Analysis of solid particle clusters in coherent structures of turbulent channel flow, SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 56(10): 2525-2530, OCT 2013

[36]Wang B, Wei W and Zhang HQ, A Study on Correlation Moments of Two-phase Fluctuating Velocity using Direct Numerical Simulation, INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 24(10), OCT 2013

[37]Zhang YL, Wang B and Zhang HQ, The Shock Wave Refraction in Supersonic Planar Mixing Layers, CHINESE PHYSICS LETTERS, 30(8), AUG 2013

[38]Lu H, Wang B and Zhang HQ, Transports of air particulate matters in the atmospheric boundary layer-numerical studies using Eulerian and Lagrangian methods, SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 56(3): 645-650, MAR 2013

[39]Liu HX, Wang B, Guo YC and Zhang HQ, Effects of Inflow Mach Number and Step Height on Supersonic Flows over a Backward-Facing Step, ADVANCES IN MECHANICAL ENGINEERING, 2013

[40]Ren ZX, Wang B and Zhang HQ, Fast Numerical Solutions of Gas-Particle Two-Phase Vacuum Plumes, ADVANCES IN MECHANICAL ENGINEERING, 2013

[41]Wang B, Zhang HQ and Wang XL, Large Eddy Simulation of Inertial Particle Preferential Dispersion in a Turbulent Flow over a Backward-Facing Step, ADVANCES IN MECHANICAL ENGINEERING, 2013

[42]Wang B, Zhang HQ and Cao HJ, Flow Dynamics of a Spiral-groove Dry-gas Seal, CHINESE JOURNAL OF MECHANICAL ENGINEERING, 26(1):78-84, JAN 2013

[43]Liang WK, Chen Z, Yang F and Zhang HQ, Effects of Soret diffusion on the laminar flame speed and Markstein length of syngas/air mixtures, PROCEEDINGS OF THE COMBUSTION INSTITUTE, 34: 695-702, 2013

[44]Zhang HQ, GaYJ, Wang B and Wang XL, Analysis of combustion instability via constant volume combustion in a LOX/RP-1 bipropellant liquid rocket engine, SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 55(4):1066-1077, APR 2012

[45]Zhang HQ, Liu M, Wang B and Wang XL, Dense gas-particle flow in vertical channel by multi-lattice trajectory model, SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 55(2):542-554, FEB 2012

[46]Zhang HQ, Yang F and Wang XL, The Effect of Soret Diffusion on Extinction Limit in Premixed and Diffusion Counterflow n-Butane/air Flames, Combustion Science and Technology,184(4):517-532, 2012

[47]Cao HJ, Zhang HQ and Lin WY, Evaluation of Presumed Probability-Density-Function Models in Non-Premixed Flames by using Large Eddy Simulation, CHINESE PHYSICS LETTERS, 29(5), MAY 2012

[48]Zhang HQ, Lu H, Wang B and Wang XL, Experimental Investigation of Flow Drag and Turbulence Intensity of a Channel Flow with Rough Walls, CHINESE PHYSICS LETTERS, 28(8), 2011,

[49]Zhang HQ, Zhou LX and Chan CK, Numerical simulation of internal flow fields of swirl coaxial injector in a hot environment, JOURNAL OF COMPUTATIONAL AND APPLIED MATHEMATICS, 235(13):3783-3790, 2011

[50]Wang B, Zhang HQ, Manhart M and Chan CK, A numerical study on statistical temporal scales in inertia particle dispersion, JOURNAL OF COMPUTATIONAL AND APPLIED MATHEMATICS, 235(13):3807-3816, 2011

[51]Yang F, Zhang HQ and Wang XL, Effects of Soret diffusion on the laminar flame speed of n-butane-air mixtures, PROCEEDINGS OF THE COMBUSTION INSTITUTE, 33:947-953, 2011

[52]Wang B and Zhang HQ, Numerical Analysis of a Spiral-groove Dry-gas Seal Considering Micro-scale Effects, CHINESE JOURNAL OF MECHANICAL ENGINEERING, 24(1):146-153, 2011

[53]Zhang HQ, Rong Y, Wang B and Wang XL, Large eddy simulation of a 3-D spatially developing turbulent round jet, SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 54(11): 2916-2923, NOV 2011

[54]Wang B, Manhart M and Zhang HQ, Analysis of inertial particle drift dispersion by direct numerical simulation of two-phase wall-bounded turbulent flows, ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS, 5(3):341-348, SEP 2011

[55]Yang F, Law CK, Sung CJ and Zhang HQ, A mechanistic study of Soret diffusion in hydrogen-air flames. Combustion and Flame, 157:192-200 , 2010

[56]Wang B, Zhang HQ and Wang XL, Evaluation of particle stochastic separated flow models via large eddy simulation, International Journal of Modern Physics C, 2010, 21(7):867-890.

[57]Wang B, Zhang HQ and Wang XL, Large-eddy Simulation of Near-field Dynamics in a Particle-laden Round Turbulent Jet, Chinese Journal of Aeronautics, 23:162-169, 2010

[58]Wang B, Manhart M and Zhang HQ, A study on turbulence modulation via an analysis of turbulence anisotropy-invariants, SCIENCE CHINA Physics, Mechanics & Astronomy, 53(3): 508–513, 2010

[59]Wang B, Zhang HQ and Wang XL, Particles modulations to turbulence in two-phase round jets, Acta Mechanica Sinica, 25(5): 611-617, 2009

[60]Wang B, Zhang HQ and Wang XL, A Time-Series Stochastic Separated Flow (TSSSF) Model for Turbulent Two-Phase Flows, Numerical Heat Transfer Part B-Fundamental, 55 (1):73-90, 2009

[61]Chen JH, Zhang HQ, Li ZY and Zhang GT, Investigation on extremal and critical characteristics of ignition time for H2/O2 combustion system and their Applications, Science in China, Series E-Technological Sciences, 52(5):1161-1166, 2009

[62]Zhang HQ, Wang B, Chan CK and Wang XL, Large Eddy Simulation of a dilute particle-laden turbulent flow over a backward-facing step, Science China Series E- Technology Science, 51 (11): 1957-1970, 2008

[63]Zhang HQ and Law CK, Effects of temporally varying liquid-phase mass diffusivity in multicomponent droplet gasification, Combustion and Flame, 153(4): 593-602, 2008

[64]Yang F, Zhang HQ, Chan CK and Wang XL, Large eddy simulation of turbulent channel flow with 3D roughness using a roughness element model, Chinese Physics Letters, 25 (1): 191-194, JAN 2008

[65]Wang B, Zhang HQ and Wang XL, Large eddy simulation of particle response to turbulence along its trajectory in a backward-facing step turbulent flow, International Journal of Heat and Mass Transfer, 49 (1-2): 415-420, 2006

[66]Cui JL, Zhang HQ, Wang B, Rong Y and Wang XL, Flow visualization and laser measurement on particle modulation to gas-phase turbulence, J. Visualization, 9(3): 339-345, 2006

[67]Liu M, Zhang HQ, Chan CK, Lau KS and Lin WY, Study of cluster formation in dense two-phase flow using a multi-lattice deterministic model, POWDER TECHNOLOGY 162 (3): 175-182, MAR 14 2006

[68]Yang WB, Zhang HQ, Chan CK, Lau KS and Lin WY, Investigation of plane mixing layer using large eddy simulation, Computational Mechanics 34 (5): 423-429 OCT 2004

[698]Wang B, Zhang HQ, Chan CK and Wang XL, Velocity fluctuations in a particle-laden turbulent flow over a backward-facing step, CMC-Computers Materials and Continua, 1 (3): 275-288 SEP 2004

[70]Yang WB, Zhang HQ, Chan CK, Lau KS and Lin WY, Large eddy simulation of mixing layer, Journal of Computational and Applied Mathematics 163 (1): 311-318 FEB 1 2004

[71]Wang B, Zhang HQ and Wang XL, Large eddy simulation of SGS turbulent kinetic energy and SGS turbulent dissipation in a backward-facing step turbulent flow, Chinese Physics Letters 21 (9): 1773-1776 SEP 2004

[72]Guo ZM, Zhang HQ, Chan CK and Lin WY, Presumed joint probability density function model for turbulent combustion, FUEL 82 (9): 1091-1101 JUN 2003

[73]Zhang HQ, Yang WB, Chan CK and Lau KS, Comparison of three separated flow models, Computational Mechanics 28 (6): 469-478 JUN 2002

[74]Zhang HQ, Zhou LX and Chan CK, A double-k-epsilon and multi-delta pdf model for turbulent gas-liquid reacting flows, FUEL 81 (6): 817-827 APR 2002

[75]Zhang HQ, Chan CK and Lau KS, Numerical simulation of sudden-expansion particle-laden flows using an improved stochastic separated flow model, Numerical Heat Transfer Part A-APPLICATIONS 40 (1): 89-102 JUL 2001

[76]Chan Ck, Zhang HQ and Lau KS, Numerical simulation of gas-particle flows behind a backward-facing step using an improved stochastic separated flow model, Computational Mechanics 27 (5): 412-417 MAY 2001

[77]Wang XL, Chan CK, Wang HY and Zhang HQ, Quantitative simulation of gas-particle two phase plane mixing layer using discrete vortex method, COMPUT MECH, 27 (5): 418-425 MAY 2001

[78]Fan QL, Wang XL, Zhang HQ and Chan CK, Large eddy simulation of a horizontal particle-laden turbulent planar jet, COMPUT MECH, 27 (2): 128-137 FEB 2001

[79]Chan CK, Zhang HQ and Lan KS, An improved stochastic separated flow model for turbulent two-phase flow, COMPUT MECH, 24 (6): 491-502 JAN 2000