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个人简介

姓    名:高振勋     教授,国家级青年人才     
所在单位:空气动力学系
研究方向计算流体力学、可压缩湍流/燃烧高精度模拟、可压缩湍流/转捩模型、高超声速气动力/热数值模拟、高温气体动力学。
邮箱:gaozhenxun@buaa.edu.cn

详细介绍

高振勋,男,1982年6月生,博士,教授,博士生导师,国家级青年人才。现任航空学院工会主席,流体所支部书记。2005年在北京航空航天大学航空科学与工程学院取得学士学位后师从李椿萱院士攻读流体力学博士学位,2011年6月获得博士学位,并于同年7月入职北京航空航天大学航空科学与工程学院任教。2015年5月至2016年4月在德国亚琛工业大学从事访问学者研究。目前承担国家一流本科课程《空气动力学》及研究生课程《计算流体力学》等教学任务。担任国家CFD2035愿景编写组的多相/多物理场方向负责人、第七届中国空气动力学会高超声速专业委员会委员、第九届航空学会气动专委会委员、《气动研究与实验》首届编委会委员、《应用力学学报》青年编委。2020年获中国力学学会科技进步二等奖(排名1),2022年获中国航空学会技术发明一等奖(排名2),2019年获中国力学学会全国徐芝纶力学优秀教师奖。

研究方向:计算流体力学、可压缩湍流/燃烧高精度模拟、可压缩湍流/转捩模型、高超声速气动力/热数值模拟、高温气体动力学。

研究经历:作为负责人承担了纵向课题20余项,包括国家自然科学基金青年基金和面上项目、国家数值风洞工程重点项目、××××重大科技工程项目、某重大基础研究项目群项目、*科技基金、国家863计划项目等,并与航天一院、航天四院、航天十一院、航空气动院等单位开展了多项型号相关课题研究。研究成果在我国多个重点飞行器研制中成功应用,有力支持了相关型号发展。

学术成果:以第一或通讯作者发表SCI论文42篇,包括Physics of Fluids、AIAA Journal、Combution and Flame、International Journal of Heat and Mass Transfer等国际权威期刊。长期担任《AIAA Journal》、《Physics of Fluids》等SCI期刊的审稿人。代表论文如下:

[1]Guo X L,Gao Z X*. A hybrid chemical source treatment for non-premixed combustion simulations.Combustion and Flame, 2023, 248: 112590.

[2]Guo P X, Shi F C,Gao Z X*, et al.Heat transfer and behavior of the Reynolds stress in Mach 6 boundary layer transition induced by first-mode oblique waves.Physics of Fluids, 2022, 34(10): 104116. (Editor’s Pick)

[3]Guo P X, Shi F C,Gao Z X*, et al.Sensitivity analysis on supersonic-boundary-layer stability: Parametric influence, optimization, and inverse design.Physics of Fluids,2022, 34(10):104113

[4]Yang Z P, Wang S Z,Gao Z X*, et al. Studies on effects of wall temperature variation on heat transfer in hypersonic laminar boundary layer.International Journal of Heat and Mass Transfer, 2022, V190: 122790

[5]Li C H, Gao Z X*, Zhao M X, et al. Compressible modification of boundary-layer momentum thickness localized method in transition model.International Journal of Heat and Fluid Flow, 2022, 98: 109068.

[6]Tian Y Y,Gao Z X*, Jiang C W, et al.A correction for Reynolds-averaged-Navier–Stokesturbulence model under the effect of shock waves inhypersonic flows.International Journal of Numerical Methods in Fluids, DOI: 10.1002/fld.5150

[7]Zhou Z F, Zhang Z C,Gao Z X*, et al.Numerical investigation on mechanisms of MHD heat fluxmitigation in hypersonic flows.Aerospace, 2022, 9: 548

[8]Mo F, Su W,Gao Z X*, et al. Numerical investigations of the slot blowing technique on the hypersonic vehicle for drag reduction.Aerospace Science and Technology,2022, V121: 107372

[9]Guo P X,Gao Z X*,Jiang C W, Lee C-H. Sensitivity analysis on supersonic-boundary-layer stability subject to perturbation of flow parameters.Physics of Fluids, 2021, 33: 084111

[10]Xu K, Li X,Gao Z X*,Jiang C W, Lee C-H.Theoretical analysis of quasi-one-dimensional compressible magnetohydrodynamic channel flow.Applied Mathematics and Computation, 2021, 411: 126500

[11]Shi F C,Gao Z X*,Jiang C W, Lee C-H.Numerical investigation of shock-turbulent mixing layer interaction and shock-associated noise.Physics of Fluids, 2021, 33: 025105.

[12]Tian Y Y, Li W H, Xue P,Gao Z X*.Numerical studies on heat transfer of supersonic, combustion-gas jets on perpendicular flat plate.Heat Transfer Engineering, 2022, 43: 864-878

[13]Lv G L,Gao Z X*,Qian Z S,Jiang C W, Lee C-H.Studies on unsteady mode transition of a turbine based vombined vycle (TBCC) inlet with multiple movable panels.Aerospace Science and Technology, 2021, 111: 106546

[14]Shi F C,Gao Z X*,Jiang C W, Lee C-H.Investigation on noise from shock/isotropic turbulence interaction using direct numerical simulation.Journal of Sound and Vibration, 2020, 488: 115633.

[15]Xu C H, Fan Y H, Wang S Z,Gao Z X*, et al.Direct numerical simulation study on the mechanisms of the magnetic field influencing the turbulence in compressible magnetohydrodynamic flow.Journal of Turbulence, 2020, 21(12): 675-703.

[16]Liu H P,Gao Z X*,Jiang C W, Lee C-H.Studies of combustion effects on near-wall turbulence in supersonic flows by large eddy simulation.Aerospace Science and Technology, 2020, 107: 106328.

[17]Wan K D, Vervisch L,Gao Z X*, et al.Development of reduced and optimized reaction mechanism for potassium emissions during biomass combustion based on genetic algorithms.Energy, 2020, 211: 118565

[18]Guo P X,Gao Z X*,Jiang C W, Lee C-H.Linear stability analysis on the most unstable frequencies of supersonic flat-plate boundary layers.Computers and Fluids,2020, 197:104394.

[19]Liu H P,Gao Z X*, Jiang C W, Lee C-H.Numerical study of combustion effects on the development of supersonic turbulent mixing layer flows with WENO schemes.Computers and Fluids, 2019, 189(15): 82-93.

[20]Guo P X,Gao Z X*, Wu Z Y, Jiang C W, Lee C-H. Investigations on the accurate prediction of supersonic shear layers for detached eddy simulation.Aerospace Science and Technology, 2019, V89: 46-57.

[21]Wu Z Y,Gao Z X*, Jiang C W, Lee C-H.An in-depth numerical investigation of a supersonic cavity-ramp flow with DDES method.Aerospace Science and Technology, 2019, V89: 253-263.

[22]Guo P X,Gao Z X*, Zhang Z C, Jiang C W, Lee C-H. Local-variable-based model for hypersonic boundary layer transition.AIAA Journal, 2019, V57(6): 2372-2383

[23]Gao Z X*,Xue H C, Zhang Z C, Liu H P,Jiang C W, Lee C H. A Hybrid Numerical Scheme for Aeroheating Computation of Hypersonic Reentry Vehicles.International Journal of Heat and Mass Transfer,2018, 116: 432-444.

[24]Jiang Y Z,Gao Z X*, Lee C H. Particle simulation of nonequilibrium gas flows based on ellipsoidal statistical Fokker–Planck model.Computers and Fluids, 2018, 170: 106-120.

[25]Li P,Gao Z X*, Lyu G L, et al. Overset structured grids assembly method for numerical simulations of multi-bodies and moving objects.Computers and Fluids, 2018, 175: 260-275

[26]Gao Z X*, Jiang C W, Lee C H. Representative interactive flamelet model and flamelet/progress variable model for supersonic combustion flows.Proceeding of the Combustion Institute,2017, V36(2): 2937-2946.

[27]Zhang Z C,Gao Z X*, Jiang C W, Lee C H. A RANS model correction on unphysical over-prediction of turbulent quantities across shockwave.International Journal of Heat and Mass Transfer,2017, V106: 1107-1119.

[28]Gao Z X*, Jiang C W, Lee C H. A new wall function boundary condition including heat release effect for supersonic combustion flows.Applied Thermal Engineering, 2016, V92: 62-70.

[29]Gao Z X*, Jiang C W, Pan S W, Lee C H. Combustion heat release effects on supersonic compressible turbulent boundary layers.AIAA Journal, 2015, V53 (7): 1949-1968.

[30]Gao Z X*, Jiang C W, Lee C H. On the laminar finite rate model and flamelet model for supersonic turbulent combustion flows.International Journal of Hydrogen Energy, 2016, V41(30): 13238-13253.

[31]Liu H P,Gao Z X*,Tang Y H,Jiang C W, Lee C H.Improvement of Skin Friction and Heat Transfer Prediction Theory of Turbulent Boundary-Layer Combustion of Hydrogen.International Journal of Hydrogen Energy, 2017, 42(41): 26123-26131.

[32]Wang J Y,Gao Z X*, Lee C H. An iterative technique for coupled conduction- radiation heat transfer in semitransparent media[J].Numerical Heat Transfer A: Applications, 2015, V67(11): 1208-1231.

[33]Jiang Y Z,Gao Z X*, Jiang C W, Lee C H. Hypersonic aeroheating characteristics of leading edges with different nose radii[J].Journal of Thermophysics and Heat Transfer, 2017, 31(3): 538-548.

[34]FanYH,Gao Z X*, Jiang C W, Lee C H.Effects of steam ingestion on underfuselage inlet performance during a catapult-assisted take-off process[J].ASME Journal of Fluids Engineering, 2018,140: 041101

[35]Gao Z X*, Cai J X, Li Jian,et al.Numerical study on mechanism of drag reduction by micro-blowing technique on supercritical airfoil[J].Journal of Aerospace Engineering,2017, 04016084.

[36]Gao Z X*,Wang J Y, Jiang C W, Lee C H. Application and theoretical analysis of the flamelet model for supersonic turbulent combustion flows in the scramjet engine[J].Combustion Theory and Modelling, 2014, V18(6): 652-691.

[37]Wang J Y,Gao Z X*, Lee C H. A decoupled procedure for convection-radiation simulation in scramjets [J].Science China Technological Science, 2014, V57(12): 2551-2566.

[38]Gao Z X*, Jiang C W, Lee C H. Improvement and application of wall function boundary condition for high-speed compressible flows[J].Science China Technological Science, 2013, V56(10):2501-2515.

[39]Tang H,Gao Z X*.Investigation of turbulence model with compressibility correction for hypersonic boundary flows[J].Advances in Mechanical Engineering, 2015, V7(12): 1-23.

[40]Gao Z X*,Lee C H. Numerical research on mixing characteristics of different injection schemes for supersonic transverse jet[J].Science China Technological Science, 2011, V54(4):883-893.

[41]Gao Z X*, Lee C H. A flamelet model for turbulent diffusion combustion in supersonic flow[J].Science China Technological Science, 2010, V53(12): 3379- 3388.

[42]Gao Z X*, Lee C H. A numerical study of turbulent combustion characteristics in a combustion chamber of a scramjet engine[J].Science China Technological Science, 2010, V53(8):2111-2121.

联系方式:

办公室:国家计算流体力学实验室(CFD楼)215室

电话:010-82315396,15901509438

E-mail:gaozhenxun@buaa.edu.cn

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