Dr Huang zhangfeng is an academic staff in the Department of Mechanics, Tianjin University, China. He has been working in Tianjin University since he obtained the bachelor’s degree, master’s degree and doctoral degree from Tianjin University. During this period, he worked as a scholar visitor in Imperial College London for one year. His major is fluid mechanics, and his main research interests include transition prediction, flow stability, transition and turbulence, direct numerical simulation, computational fluid dynamics, etc.

He has been engaged in the theoretical study of flow stability, transition mechanism and turbulence for more than 20 years, and has made many achievements in these fields. He has published more than 30 high-level papers. Among them, there are five articles in the top international journals in the field of fluid mechanics, including two articles in Journal of Fluid Mechanics, two articles in Physics of Fluids, one article in Physical Review Fluids. And there are seven articles in the top domestic journals, including one article in Chinese Journal of Aeronautics, two articles in Applied Mathematics and Mechanics (English Edition), four articles in Science China-Physics Mechanics & Astronomy.

He has been devoted himself to the engineering application of transition prediction for nearly 10 years. He developed an engineering oriented software of transition prediction, and promoted it to the engineering application department. He has taken charge of more than 40 projects, including one project from “National Numerical Wind-tunnel”, three projects from “National Natural Science Foundation of China”. He has secured more than ten million of RMB in research funding, including three projects more than one million. He was recognized by the engineering application department.

His major academic contributions are: (1) He revealed the transition mechanism and fully developed turbulent characteristics of supersonic boundary layer on flat plate; (2) He improved the linear stability theory by extending the traditional theory based on parallel flow hypothesis to nonparallel flow and local abrupt flow; (3) He proposed the concept of damped wave and quantitatively provided the receptivity coefficient of an oblique shock wave over two-dimensional free-stream disturbances; (4) He improved the application ability of the transition prediction eN method in three-dimensional boundary layers by proposing the concept of generalized growth rate and developing parabolic stability equation based on ray tracing theory.

He is a member of American Institute of Aeronautics and Astronautics, China Society of Theoretical and Applied Mechanics, Chinese Aerodynamics Society. He is a scientific editor of Acta Aerodynamica Sinica, and a youth scientific editor of Journal of Experiments in Fluid Mechanics. He is a reviewer of more than 10 journals, such as Physics of Fluids, Applied Mathematics and Mechanics (English Edition), Advances in Applied Mathematics and Mechanics, Chinese Journal of Aeronautics. He is supervising/has supervised five doctoral students and thirteen master’s students, two of whom have won the title of outstanding graduates (top 10%).

• 工程转捩预测
• 流动稳定性
• 转捩与湍流
• 直接数值模拟

• 天津大学青年教工先锋岗 (2012)
• 天津大学青年骨干教师 (2010)
• 天津大学本科生毕业设计（论文）优秀指导教师 (2010)
• 全国优秀博士论文提名 (2009)
• 天津市优秀博士论文(2009)
• 天津大学优秀博士论文(2008)

• Huang Zhangfeng*, Wang Huilin. Linear interaction of two-dimensional free-stream disturbances with an oblique shock wave. Journal of Fluid Mechanics, 2019, 873:1179-1205. https://doi.org/10.1017/jfm.2019.438.
• Huang Zhangfeng, Wu Xuesong*. A local scattering approach for the effects of abrupt changes on boundary-layer instability and transition: A finite-Reynolds-number formulation for isolated distortions. Journal of Fluid Mechanics, 2017, 822:444-483. https://doi.org/10.1017/jfm.2017.287.
• Huang Zhangfeng*, Wu Xuesong. A non-perturbative approach to spatial instability of weakly non-parallel shear flows. Physics of Fluids, 2015, 27, 054102:1-21. https://doi.org/10.1063/1.4919957.
• Song Run Jie, Zhao Lei, Huang Zhangfeng*. Secondary instability of stationary Görtler vortices originating from first/second Mack mode. Physics of Fluids, 2020, 32, 000000:1-17. https://doi.org/10.1063/1.5140222.
• Song Run Jie, Zhao Lei, Huang Zhangfeng*. Improvement of the parabolized stability equation to predict the linear evolution of disturbances in three-dimensional boundary layers based on ray tracing theory. Physical Review Fluids, 2020, 5, 033901:1-21. https://doi.org/10.1103/PhysRevFluids.5.033901.
• Song Run Jie, Zhao Lei, Huang Zhangfeng*. Conservation relation of generalized growth rate in boundary layers. Applied Mathematics and Mechanics (English Edition), 2018,29(12):1755-1768. https://doi.org/10.1007/s10483-018-2394-9.
• Jing Zhenrong, Huang Zhangfeng*. Instability Analysis and Drag Coefficient Prediction on a Swept RAE2822 Wing with Constant Lift Coefficient. Chinese Journal of Aeronautics, 2017, 30(3):964-975. http://dx.doi.org/10.1016/j.cja.2017.03.002.
• Huang Zhangfeng, Liu Zhengxian*. Numerical study of a positive displacement blower. Proceedings of the Institution of Mechanical Engineers Part C-Journal of Mechanical Engineering Science, 2009. 223(5):2309-2316. http://dx.doi.org/10.1243/09544062JMES1503.
• Huang Zhangfeng, Zhou Heng*. Inflow conditions for spatial direct numerical simulation of turbulent boundary layers. Science China-Physics Mechanics & Astronomy, 2008, 51(8):1106-1115. https://doi.org/10.1007/s11433-008-0093-7. 黄章峰, 周恒*. 湍流边界层的空间模式DNS的入口条件. 中国科学 G辑 物理学 力学 天文学, 2008, 38(3):310-318. https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFD2008&filename=JGXK200803010.
• Huang Zhangfeng, Zhou Heng *. The investigation of coherent structures in the wall region of a supersonic turbulent boundary layer based on DNS database. Science China-Physics Mechanics & Astronomy, 2007, 50(3):348-356. https://doi.org/10.1007/s11433-007-0024-z. 黄章峰, 周恒*. 基于DNS数据库的超音速湍流边界层近壁区相干结构的研究. 中国科学 G辑 物理学 力学 天文学, 2006, 36(6):653-661. https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFD2006&filename=JGXK200606008.
• Huang Zhangfeng, Zhou Heng*, Luo Jisheng. Direct numerical simulation of a supersonic turbulent boundary layer on a flat plate and its analysis. Science China-Physics Mechanics & Astronomy, 2005, 48(5):626-640. https://link.springer.com/article/10.1360/142005-184. 黄章峰, 周恒*, 罗纪生. 超音速平板边界层湍流的直接数值模拟及分析. 中国科学 G辑 物理学 力学 天文学, 2006, 36(1):46-58. https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFD2006&filename=JGXK200601004.
• Huang Zhangfeng, Cao Wei, Zhou Heng*. The mechanism of breakdown in laminar-turbulent transition of a supersonic boundary layer on a flat plate-temporal mode. Science China-Physics Mechanics & Astronomy, 2005, 48(5):614-625. https://link.springer.com/article/10.1360/142005-19. 黄章峰, 曹伟, 周恒*. 超音速平板边界层转捩中层流突变为湍流的机理—时间模式. 中国科学 G辑 物理学 力学 天文学, 2005, 35(5):537-547. https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFD2005&filename=JGXK200505009.
• Huang Zhangfeng, Zhou Heng*. Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets. Applied Mathematics and Mechanics (English Edition), 2004, 25(1):1-9. https://doi.org/10.1007/BF02437288. 黄章峰*, 周恒. 超音速边界层中二维扰动的演化及小激波的产生. 应用数学和力学, 2004, 25(1):1-8. https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFD2004&filename=YYSX200401001, https://doi.org/10.3321/j.issn:1000-0887.2004.01.001.
• Huang Zhangfeng*, Zhang Panfeng, Zhan Shige. Review of the tenth national symposium on fluid mechanics for young scholars. Chinese Journal of Theoretical and Applied Mechanics, 2017, 49( 6):1428-1434. http://dx.doi.org/10.6052/0459-1879-17-313. 黄章峰*, 张攀峰, 詹世革. 第十届全国流体力学青年研讨会简介. 力学学报, 2017, 49(6):1428-1434.
• Jing Zhenrong, Sun Pengpeng, Huang Zhangfeng*. Effect of attack angle on stability and transition in a swept-wing boundary layer. Journal of Beijing University of Aeronautics and Astronautics, 2015,41(11):2177-2183. http://dx.doi.org/10.13700/j.bh.1001-5965.2014.0769. 靖振荣, 孙朋朋, 黄章峰*. 小攻角对后掠机翼边界层稳定性及转捩的影响. 北京航空航天大学学报, 2015,41(11):2177-2183.
• Sun Pengpeng, Huang Zhangfeng*. Effect of sweep angle on stability and transition in a swept-wing boundary layer. Journal of Beijing University of Aeronautics and Astronautics, 2015,41(7):1313-1321. http://dx.doi.org/10.13700/j.bh.1001-5965.2014.0540. 孙朋朋, 黄章峰*. 后掠角对后掠机翼边界层稳定性及转捩的影响. 北京航空航天大学学报, 2015, 41(7):1313-1321.
• Li Hui, Huang Zhangfeng*. Effect of local hump on stability of compressible boundary layer on flat plate. Journal of Aerospace Power, 2015,30(1):173-181. http://dx.doi.org/10.13224/j.cnki.jasp.2015.01.024. 李慧, 黄章峰*. 局部凸起对可压缩平板边界层稳定性的影响. 航空动力学报, 2015, 30(1):173-181.
• Lu Xuezhi, Huang Zhangfeng*, Luo Jisheng. Application of inflow boundary conditions for DNS on bypass transition. ACTA Aerodynamica Sinica, 2012, 30(6):749-753. https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFD2012&filename=KQDX201206011. 逯学志, 黄章峰*, 罗纪生. 湍流入流条件在强迫转捩研究中的应用. 空气动力学学报, 2012,30(6):749-753.
• Huang Zhangfeng*, Wu Xuesong. The effect of local steady suction on the stability and transition of boundary layer on a flat plate. 2016, AIAA paper 2016-3471. 8th AIAA Flow Control Conference, 2016-07-13~17,Washington, D.C. oral report. http://dx.doi.org/10.2514/6.2016-3471.
• Jing Zhenrong, Huang Zhangfeng*. Instability analysis and transition prediction on a swept RAE2822 airfoil with constant lift coefficient. 2016, AIAA paper 2016-3790. 44th AIAA Fluid Dynamics Conference, 2016-07-13~17,Washington, D.C. oral report. http://dx.doi.org/10.2514/6.2016-3790.
• Huang Zhangfeng*, Wu Xuesong. A local scattering approach for the effect of abrupt changes on boundary-layer instability and transition: a numerical method. 2015, AIAA paper, 2015-2623. 45th AIAA Fluid Dynamics Conference, 2015-06-22~26, Dallas, TX, oral report. http://dx.doi.org/10.2514/6.2015-2623.
• Huang Zhangfeng*, Wu Xuesong. Non-parallel-flow effect on compressible boundary layer on a flat plate. Procedia Engineering, 2015, 126:78-82. 7th International Conference on Fluid Mechanics, ICFM 2015, 2015-05-24~27, Qingdao, China. oral report. http://dx.doi.org/10.1016/j.proeng.2015.11.182.
• Huang Zhangfeng*, Wu Xuesong. On non-parallel-flow effects on boundary-layer instability: a non-perturbative approach based on local expansion, 2014, AIAA paper, 2014-2884. 44th AIAA Fluid Dynamics Conference, 2014-06-16~20, Atlanta, GA, oral report. http://dx.doi.org/10.2514/6.2014-2884.