刘建

副教授 硕士生导师

入职时间：2020-05-14

所在单位：航空航天学院

职务：动力与控制所副所长

学历：博士研究生毕业

办公地点：中南大学本部升华楼后楼706

性别：男

联系方式：jian.liu@csu.edu.cn

学位：工学博士学位

学科：动力工程及工程热物理
航空宇航科学与技术

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个人简介

刘建，瑞典隆德大学博士及博士后，航空航天技术研究院特聘副教授。长期从事空天发动机热管理，涡轮叶片冷却、超燃冲压发动机再生冷却、超声速流动燃烧计算等研究工作。目前已发表SCI期刊论文60余篇，国际会议论文10余篇，英文著作3部，中文专著1部，国际会议特邀报告2次，获得Aerospace期刊评选的“2023 Young Investigator Award”（每年评选1人）。论文主要发表在Int. J. Heat Mass Transfer, ASME J. Heat Transfer, Int. C. Heat Mass Transfer, Int. J. Thermal Sciences, Applied Thermal Engineering, Energy, Numerical Heat Transfer, Part A等传热能源领域权威期刊，1篇论文入选ESI高被引用论文。目前Google总被引用1100余次，h-index20，以第一作者授权发明专利4项，国际专利2项；主持装备预研、湖南省揭榜挂帅项目、湖南省自然科学基金、哈尔滨工程大学、国防科技大学、航天工程大学等项目10余项，项目总经费400余万元。担任Aerospace, Energies, Foundations等国际期刊编委；担任IJHMT、ATE、IJTS等十余种国际期刊审稿人。


学习工作经历

  • 2020.05 – 至今 中南大学航空航天学院特聘副教授。 

  • 2019.05 - 2019.09 博士后 瑞典Lund University能源科学系。 

  • 2015.09 - 2019.05 博士 瑞典Lund University (2022QS排名世界87)能源科学系，导师为Bengt Sunden教授。 

  • 2014.04 - 2014.09 交流学习 美国University of Minnesota，导师为传热顶级期刊ASME J. Heat Transfer的主编，Terrence W. Simon教授。 

  • 2012.09 - 2015.03  硕士  西北工业大学  航空宇航制造工程。

  • 2008.09 - 2012.07  本科  西北工业大学  飞行器制造工程。


代表性论文

第一作者或通讯作者论文

  1. Jian Liu，Mengyao Xu, Wenjie Guo, Wenxiong Xi*, Chaoyang Liu, Bengt Sunden, Flow and heat transfer mechanism of a regenerative cooling channel mounted with pin-fins using supercritical CO2 as coolant. International Journal of Thermal Sciences, 2025, 208, 109425.

  2. Mengyao Xu, Jian Liu *, Wenxiong Xi, Chaoyang Liu, Bengt Sunden, Thermodynamic performance and flow structures analysis of supercritical CO2 applied in a regenerative cooling channel mounted with mini-ribs. Case Studies in Thermal Engineering, 2024, 60, 104704.

  3. Xirui Zhang, Rongdi Zhang, Qihan Shao, Wenxiong Xi, Jian Liu*, Bengt Sunden. Recent development of heat transfer and fluid flow of Supercritical CO2 in tubes: mechanisms and applications. Journal of Thermal Science, 2024, accepted.

  4. Xi, W.; Liu, P.; Shao, Q.; Guo, W.; Liu, J*. Parametric Study of Flow and Combustion Characteristic in a Cavitied Scramjet with Multi-Position Injection. Fire, 2024, 7, 176. 

  5. Xi, W.; Liu, P.; Zhang, R.; Dong, T.; Liu, J*. Numerical Investigation of Flow Structures and CombustionMechanisms with Different Injection Locations in a Hydrogen-Fueled Scramjet Combustor. Fire, 2024, 7, 191.

  6. Zhang, R.; Liu, P.; Zhang, X.; Xi, W.; Liu, J*. Recent Developments in the Aerodynamic Heat Transfer and Cooling Technology of Gas Turbines Endwalls. Aerospace 2023, 10, 702. 

  7. Xi, W.; Xu, H.; Dong, T.; Lin, Z.; Liu, J*. Numerical Investigation of Combustion Mechanism with Multi-Position Injection in a Dual-Mode Combustor. Aerospace 2023, 10, 656.

  8. Liu, J.; Xu, M.; Xi, W.*. Effects of Gas Thermophysical Properties on the Full-Range Endwall Film Cooling of a Turbine Vane. Aerospace 2023, 10, 592.

  9. Liu, J.; Xu, M.; Liu, P.; Xi, W.*. Heat Transfer and Flow Structure Characteristics of Regenerative Cooling in a Rectangular Channel Using Supercritical CO2. Aerospace 2023, 10, 564.

  10. He, N.; Liu, C.*; Pan, Y.; Liu, J*. Progress of Coupled Heat Transfer Mechanisms of Regenerative Cooling System in a Scramjet. Energies 2023, 16, 1025.

  11. Liu, J.; Xu, M.; Zhang, R.; Zhang, X.; Xi, W*. “Progress of Porous/Lattice Structures Applied in Thermal Management Technology of Aerospace Applications.”Aerospace 2022, 9, 827.

  12. Xi W, Xu M, Ma K, Liu J*, “Heat transfer enhancement methods applied in energy conversion storage and propulsion systems”, Energies, 2022, 15, 7218.

  13. Xi W, Xu M, Liu C, Liu J*, "Recent Developments of Heat Transfer Enhancement and Thermal Management Technology", Energies, 2022, 15, 6043. 

  14. Liu J, Xu M, Ma K, Liu C, Xi W*, "Heat Transfer and Flow Structures of Supercritical n-decane in a Regenerative Cooling Channel Loaded with Non-Uniform Heat Flux", Frontiers in Energy Research, 2022, 10:985220.

  15. Song J, Yuan Y, Liu J*, Luo S, Sunden B, "Heat Transfer  Enhancement of Regenerative Cooling Channel with Pyramid Lattice Sandwich Structures", Heat Transfer Engineering, Vol.44, 2022, 10.1080/01457632.2022.2127049.

  16. Xi W, Xu M, Liu C, Liu J*, Sunden B. Generation and Propagation Characteristics of an Auto-Ignition Flame Kernel Caused by the Oblique Shock in a Supersonic Flow Regime[J]. Energies, 2022, 15(9): 3356.

  17. Liu J, Xu M, Xi W*, Song J, Luo S and Sunden B*. Numerical investigations of endwall film cooling design of a turbine vane using four-holes pattern[J]. International Journal of Numerical Methods for Heat & Fluid Flow, Vol. 32 No. 6, 2022, pp. 2177-2197.

  18. Wenxiong, Xi, Liu Jian*, and Ren Mengfei. "Improvement of mixing efficiency in the combustion chamber of a powder-fuel ramjet engine." Frontiers in Energy Research (2021): 538.

  19. Luo, S., Miao, Z., Liu, J.*, Song, J., Xi, W., & Liu, C. (2021). Effects of Coolants of Double Layer Transpiration Cooling System in the Leading Edge of a Hypersonic Vehicle. Frontiers in Energy Research (2021) 530.

  20. Liu J, Du W, Hussain S, et al. Endwall film cooling holes design upstream of the leading edge of a turbine vane[J]. Numerical Heat Transfer, Part A: Applications, 2021, 79(3): 222-245.

  21. J. Liu, S. Hussain, W. Wang, G. Xie, B. Sundén, Experimental and Numerical Investigations of Heat Transfer and Turbulent Flow in a Rectangular Channel Mounted with Perforated Ribs,  International communications in Heat Mass Transfer, 121 (2021) Paper No. 105083.

  22. J. Liu, S. Hussain, W. Du, L. Wang, G. Xie, B. Sundén, Design of Full-scale Endwall Film Cooling of a Turbine Vane, ASME J. Heat Transfer 142 (2020) 022201.

  23. J. Liu, S. Hussain, W. Wang, L. Wang, G. Xie, B. Sundén, Effect of the Relative Location of a Pocket Cavity on Heat Transfer and Flow Structures of the Downstream Endwall with a Symmetrical Vane, International Journal of Thermal Sciences 145 (2019) 106012.

  24. J. Liu, S. Hussain, W. Wang, L. Wang, G. Xie, B. Sundén, Heat Transfer Enhancement and Turbulent Flow in a Rectangular Channel Using Perforated Ribs with Inclined Holes, ASME Journal of Heat Transfer 141 (2019) paper No. 041702.

  25. J. Liu, S. Hussain, L. Wang, G. Xie, B. Sundén, Effects of a Pocket Cavity on Heat Transfer and Flow Characteristics of the Endwall with a Bluff Body in a Gas Turbine Engine, Applied Thermal Engineering 143 (2018) 935-946.

  26. J. Liu, S. Hussain, C. Wang, L. Wang, G. Xie, B. Sundén, Effects of the Pocket Cavity on Heat Transfer and Fluid Flow of the Downstream Outlet Guide Vane at Different Flow Attacking Angles, Numerical Heat Transfer, Part A: Applications 74 (2018) 1087-1104.

  27. J. Liu, S. Hussain, J. Wang, L. Wang, G. Xie, B. Sundén, Application of Fractal Theory in the Arrangement of Truncated Ribs in a Rectangular Cooling Channel (4:1) of a Turbine Blade, Applied Thermal Engineering 139 (2018) 488-505.

  28. J. Liu, S. Hussain, J. Wang, L. Wang, G. Xie, B. Sundén, Heat transfer enhancement and turbulent flow in a high aspect ratio channel (4: 1) with ribs of various truncation types and arrangements, International Journal of Thermal Sciences 123 (2018) 99-116. (ESI高倍引论文)

  29. J. Liu, G.N. Xie, B. Sunden, Flow pattern and heat transfer past two tandem arranged cylinders with oscillating inlet velocity, Applied Thermal Engineering 120 (2017) 614-625.

  30. J. Liu, S. Hussain, L. Wang, G. Xie, B. Sundén, Heat transfer and turbulent flow characteristics over pocket cavity in the junction part of an outlet guide vane in a gas turbine, Applied Thermal Engineering 124 (2017) 831-843.

  31. J. Liu, G. Xie, B.A. Sunden, L. Wang, M. Andersson, Enhancement of heat transfer in a square channel by roughened surfaces in rib-elements and turbulent flow manipulation, International Journal of Numerical Methods for Heat & Fluid Flow 27 (2017) 1571-1595.

  32. J. Liu, G. Xie, T.W. Simon, Turbulent flow and heat transfer enhancement in rectangular channels with novel cylindrical grooves, International Journal of Heat and Mass Transfer 81 (2015) 563-577. 

  33. J. Liu, Y. Song, G. Xie, B. Sunden, Numerical modeling flow and heat transfer in dimpled cooling channels with secondary hemispherical protrusions, Energy 79 (2015) 1-19.