个人简介
姓名：高振勋副教授
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/燃烧大涡模拟
邮箱：gaozhenxun@buaa.edu.cn

详细介绍 高振勋，男，1982年6月生，博士，副教授，空气动力学系书记。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研究。目前承担本科生《空气动力学》及研究生《现代飞机设计空气动力学》等课程的教学任务。担任第七届中国空气动力学会高超声速专业委员会委员

研究方向：计算流体力学、可压缩湍流/燃烧大涡模拟、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12项，包括国家自然科学基金1项、×××× 重大专项课题1项、军委科技委国防科技基金1项，863课题4项、航空基金课题1项，并与航天一院、航天四院、航天五院、沈阳飞机设计研究所等单位开展了多项横向课题研究。此外，还参与其它多项研究课题，包括国家重大专项课题以及973项目等。

学术成果：共发表SCI论文25篇，第一或通讯作者发表SCI论文18篇(Q1区文章7篇），EI文章12篇，其它会议文章多篇。长期担任SCI期刊《AIAA Journal》、、《Aerospace Science andTechnology》、《EngineeringApplications of Computational Fluid Mechanics》和EI期刊《推进技术》、《西安交通大学学报》的审稿人。代表论文如下：
[1] Gao Z X*, Jiang C W, Lee C H. Representativeinteractive flamelet model and flamelet/progress variable model for supersoniccombustion flows. Proceeding of the Combustion Institute, 2017, V36(2):2937-2946. (IF= 3.214)
[2] 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 HypersonicReentry Vehicles. International Journal of Heat and Mass Transfer, 2017,in print. (IF= 3.458)
[3] Zhang Z C, Gao Z X*,Jiang C W, Lee C H. A RANS model correction on unphysical over-prediction ofturbulent quantities across shockwave. International Journal of Heat andMass Transfer, 2017, V106: 1107-1119. (IF= 3.458)
[4] Gao Z X*, Jiang C W, Lee C H. A new wall functionboundary condition including heat release effect for supersonic combustionflows. Applied Thermal Engineering, 2016, V92: 62-70. (IF= 3.356)
[5] Gao Z X*, Jiang C W, Pan S W, Lee C H. Combustionheat release effects on supersonic compressible turbulent boundary layers. AIAAJournal, 2015, V53 (7): 1949-1968. (IF= 1.638)
[6] Gao Z X*, Jiang C W, Lee C H. On the laminarfinite rate model and flamelet model for supersonic turbulent combustion flows.International Journal of Hydrogen Energy, 2016, V41(30): 13238-13253.(IF= 3.582)
[7] Liu H P, Gao Z X*,Tang Y H, Jiang C W, Lee C H. Improvement of Skin Friction and Heat TransferPrediction Theory of Turbulent Boundary-Layer Combustion of Hydrogen.International Journal of Hydrogen Energy, 2017, in print. (IF= 3.582)
[8] Wang J Y, Gao Z X*,Lee C H. An iterative technique for coupled conduction- radiation heat transferin semitransparent media[J]. Numerical Heat Transfer A: Applications,2015, V67(11): 1208-1231. (IF= 2.259)
[9] Jiang Y Z, Gao Z X*,Jiang C W, Lee C H. Hypersonic aeroheating characteristics of leading edgeswith different nose radii[J]. Journalof Thermophysics and Heat Transfer, doi: 10.2514/1.T4950. (IF= 1.315)
[10] Fan Y H, Gao Z X*,Jiang C W, Lee C H. Effects of steam ingestion on underfuselage inletperformance during a catapult-assisted take-off process[J]. ASME Journal ofFluids Engineering, 2017, in print. (IF= 1.437)
[11] Gao Z X*, Cai J X, Li Jian, et al. Numerical study on mechanism of drag reduction by micro-blowingtechnique on supercritical airfoil[J]. Journal of Aerospace Engineering,doi:10.1061/(ASCE)AS.1943-5525.**.(IF= 1.107)
[12] Gao Z X*, Wang J Y, Jiang C W, Lee C H.Application and theoretical analysis of the flamelet model for supersonicturbulent combustion flows in the scramjet engine[J]. Combustion Theory andModelling, 2014, V18(6): 652-691. (IF= 1.855)
[13] 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. (IF=1.719)
[14] Gao Z X*, Jiang C W, Lee C H. Improvement and application of wall functionboundary condition for high-speed compressible flows[J]. Science ChinaTechnological Science, 2013, V56(10):2501-2515. (IF= 1.719)
[15] Tang H, Gao Z X*. Investigation of turbulence model withcompressibility correction for hypersonic boundary flows[J]. Advancesin Mechanical Engineering, 2015, V7(12): 1-23. ((IF= 0.827)
[16] Gao Z X*, Lee C H. Numericalresearch on mixing characteristics of different injection schemes forsupersonic transverse jet[J]. Science China Technological Science, 2011,V54(4):883-893. (IF= 1.719)
[17] Gao Z X*, Lee C H. A flamelet model for turbulent diffusion combustion insupersonic flow[J]. Science China Technological Science, 2010, V53(12):3379- 3388. (IF= 1.719)
[18] Gao Z X*, Lee C H. A numerical study of turbulent combustion characteristics ina combustion chamber of a scramjet engine[J]. Science China TechnologicalScience, 2010, V53(8):2111-2121. (IF= 1.719)


联系方式：
办公室：国家计算流体力学实验室（CFD楼）205室
电话：，**
E-mail:gaozhenxun@buaa.edu.cn