• Papers

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• [1] Huang Zhengfeng*, 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.
• [2] 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.
• • [3] 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.
  • [4] Song Runjie, Zhao Lei, Huang Zhangfeng*. Secondary instability of stationary Görtler vortices originating from first/second Mack mode. Physics of Fluids, 2020, 32, 034109:1-17. https://doi.org/10.1063/1.5140222.
  • [5] Song Runjie, 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.
  • [6] Song Runjie, 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.
  • [7] 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.
  • [8] 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.
  • [9] 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.
  • [10] 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.
  • [11] 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.
  • [12] 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.
  • [13] 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.
  • [14] 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.
  • [15] 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.
  • [16] 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.
  • [17] 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.
  • [18] 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.
  • [19] 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.
  • [20] 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.
  • [21] 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.
  • [22] 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.
  • [23] 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.

• Honors & Awards

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• [1] Young faculty pioneer of Tianjin University (2012)
• [2] Young backbone teachers of Tianjin University (2010)
• • [3] Excellent instructor of graduation project (Thesis) of Tianjin University (2010)
  • [4] Nomination of National Excellent Doctoral Dissertation (2009)
  • [5] Excellent Doctoral Dissertation of Tianjin (2009)
  • [6] Excellent Doctoral Dissertation of Tianjin University (2008)

• Projects

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• [1] National Numerical Wind-tunnel
• [2] National Natural Science Foundation of China
• • [3] Tianjin Natural Science Foundation
  • [4] Specialized Research Fund for the Doctoral Program of Higher Education of China
  • [5] China Postdoctoral Science Foundation
  • [6] Open fund from State Key Laboratory of Aerodynamics