Liu Huaping

    Associate professor

    Phone:86-18804639176

    Email:hgdlhp@163.com





Research Interests:

Ø Aerodynamics in turbomachinery

    l Design of highly loading compressor cascade

    l Loss mechanism in turbomachinery

Ø Flow control technology, e. g. Plasma actuation, Boundary layer suction

Ø Supersonic Aerodynamics

Ø Multiphase flow, e. g. SupercavitationFree surface flow, Phase change


Academic Degrees: PhD in Power Machinery and Engineering


Educational experience:

Ø March 2008~July 2011: Ph.D. In Power Machinery and Engineering, Harbin Institute of Technology, Harbin, China (Advisors: Drs. Chen Fu & Song Yan-ping, Harbin Institute of Technology, Harbin, China; Dissertation: The DBD plasma effect on the boundary layer separation)

Ø June 2006~March 2008: Master degree candidate. In Power Machinery and Engineering, Harbin Institute of Technology, Harbin.

Ø Sept. 2002~July 2006: B.Sc. In School of Energy Science and Engineering, Harbin Institute of Technology, Harbin.


Selected Publications

[1] H Liu Y Yu H Chen M Yu D Zhang. A parametric investigation of endwall vortex generator jet on the secondary flow control for a high turning compressor cascade. Journal of Thermal Science & Technology, 2017, 12 (1): JTST0006-JTST0006. (SCI).

[2] H Liu D Zhang YU Yongchuan H Chen. Separation control with endwall corner jet in a high-speed compressor cascade. Journal of Thermal Science & Technology, 2017, 12 (2), DOI: 10.1299/jtst.2017jtst0019. (SCI).

[3] H Liu S Jiang Y Yu D Zhang H Chen. Secondary flow control using endwall jet fence in a high-speed compressor cascade. Journal of Mechanical Science & Technology, 2017, 31 (10):4841-4852. (SCI).

[4] H Liu Y Qin R Wang D Zhang B Lu. The Performance of the Self-Supplying Vortex Generator Jets on a High-Speed Compressor Cascade. International Journal of Turbo & Jet-Engines, 2016. (SCI)

[5] Huaping Liu, Yongchuan Yu, Feipeng Yu, Dongfei Zhang and Huanlong Chen. A Parametric Investigation of Wake Loss Reduction by using Serrated Trailing Edge in a High-speed Compressor Cascade. INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2017.12. (SCI).

[6] Jianyang YU, Huaping LIU (通讯作者), Ruoyu WANG and Fu CHEN. Numerical study of the flow structures in flat plate and the wall-mounted hump induced by the unsteady DBD plasma. Plasma Sci. Technol. 2017, 19, 015502. (SCI)

[7] Xiao-di WU, Hua-ping LIU, Fu CHEN. Numerical investigation of flow characteristics around two side-by-side cylinders by immersed boundary-lattice Boltzmann flux solver. J Zhejiang Univ-Sci A (Appl Phys & Eng), 2017,12 (on line). (SCI)

[8] 刘华坪李得英陈焕龙张东飞. Effects of Vortex Generator Jet on Corner Separation/Stall in High-Turning Compressor Cascade. Transactions of Tianjin University, 2016, 22(6): 555-562. (EI

[9] Huaping Liu, B.-X. Lu. End-wall flow control in a high speed compressor cascade using vortex generator jet. Proceedings of ASME Turbo Expo 2016: Turbine Technical Conference and Exposition, 2016 (EI