2011-2016 bat365在线中国官网登录入口 动力工程及工程热物理专业 博士
2015.04-2015.10 牛津大学 工程系 联合培养博士生
2007-2011 山东大学 机械工程专业 学士

2022.01-至今 bat365在线中国官网登录入口 副教授、硕导、博导
2019.02-2021.12 bat365在线中国官网登录入口 助理教授、硕导、博导
2018.01-2019.01 牛津大学工程系 博士后研究员
2016.10-2017.12 西门子公司中央研究院 研发工程师

1. 航空发动机和燃气轮机涡轮的冷却、传热和流动：响应国家“航空发动机和燃气轮机”重大科技战略，开展涡轮叶片气膜冷却和新型热流测试方法（高频快响测温、红外成像测温、磁共振成像测速）的研究。
2. 高速飞行器及其动力系统的气动热防护：面向可重复、宽速域空天飞行的前瞻技术需求，开展高速飞行器气膜冷却、激波管风洞实验、主动流动控制等新技术的研究。
3. 智能热管理与流动控制：应用人工智能/机器学习的最新算法，针对能源动力、航空航天领域的实际工程问题，开展热管理与流动控制的设计优化研究。
4. 临床医学与热流体工程的学科交叉研究：面向医学工程和生命健康的技术需求，开展血流动力学、血管支架设计等新型诊疗方法的研究。

常年招收博士、硕士研究生及本科实习生，欢迎对以上研究方向感兴趣的同学联系！

Chair of Facilities and Instrumentation Session, International Symposium on Shock Waves, 2023
Chair of Heat Transfer Session, ASME Turbo Expo, 2019
Chair of Heat Transfer Session, Global Power and Propulsion Forum, 2017, 2022
分会主席（涡轮冷却），中国工程热物理年会热机气动力学分会，2020
Reviewer for:
International Journal of Thermal Sciences, International Journal of Heat and Mass Transfer, Physics of Fluids, ASME Journal of Thermal Science and Engineering Applications, Journal of Power and Energy, Journal of Aerospace Engineering, Aeronautical Journal, ASME Turbo Expo, etc.

2023-2024 国防科技创新特区先进航空动力创新工作站项目，负责人
2022-2024 中国科协青年人才托举工程项目，负责人
2022-2024 国家自然科学基金，高压涡轮叶顶激波与冷却射流相互作用的机理研究，负责人
2021-2024 上海市自然科学基金，跨声速内流中激波与气膜冷却的相互作用机理及气热一体化调控，负责人
2021-2023 中国航天科技集团第八研究院产学研合作基金，负责人
2021-2023 bat365在线中国官网登录入口医工交叉研究基金，合作者（Co-PI）
2020-2023 上海市青年科技英才扬帆计划，跨音速高压涡轮叶顶间隙中激波气热特性的实验研究，负责人
2019-2022 bat365在线中国官网登录入口新进教师科研启动项目，自然对流的传热流动机理及其在余热回收中的应用，负责人

2021-2023 中国航发湖南动力机械研究所（608），某涡轴发动机涡轮工作叶片小翼叶尖流动及换热特性试验研究，主要参与人
2018-2019 英国EPSRC项目，Geothermally Sourced Combined Power and Freshwater Generation for Eastern Africa，主要参与人
2014-2016 国家自然科学基金，跨音高速旋转工况下高压涡轮凹槽叶尖冷却的实验研究，主要参与人
2011-2013 国家自然科学基金，透平动叶顶部间隙跨音流场对气动传热的影响，主要参与人
2012-2014 中国航发商用航空发动机公司，高压涡轮动叶叶顶泄漏情况下的叶尖冷却换热研究，主要参与人

2024年
1. Zeng, W., Ma, H.*, 2024, "Physical Mechanism for Extending the Test Time in Gun Tunnels," Aerospace Science and Technology, Vol. 146, pp. 108920 (11 pages)
2. Dai, S., Ma, H.*, Xu, Z., Feng, K., 2024, “Numerical Study of Discrete Film Cooling Near the Rudder Shaft of a Hypersonic Air Fin Model,” Numerical Heat Transfer, Part A: Applications, Vol. 85, No. 5, pp. 679-701

2023年
1. Ma, H., Liu, Y., Lai, Y., Ouyang, H.*, Ning, J., Jiang, X., Xu, Q., 2023, "Magnetic Resonance Velocimetry of A Turbine Blade With Engine Representative Internal and Film Cooling Structures," ASME Journal of Turbomachinery, Vol. 145, No. 1, pp. 011004 (10 pages)
2. Jianing Li, Zhipeng Zong, Tao Zhou, Jiang Zhang, Haiteng Ma*, 2023, "Hemodynamics in Portal Venous Based on 9.4T Magnetic Resonance Velocimetry and Numerical Simulations", Journal of Shanghai Jiao Tong University, Accepted
3. 赖佑奎,马海腾,刘一粟,欧阳华*.基于磁共振测速的复合冷却涡轮叶片流动分析.航空学报,2023, 44(14): 627920-627920
4. 戴思明, 许自然, 窦怡彬, 马海腾*, 赵如意, 2023, "超高速流动中气膜冷却技术的研究综述," 空天防御, 6(4), pp. 24-29.
5. 刘一粟, 曾伟, 戴思明, 李家宁, 马海腾*.跨音速槽道流中绝热气膜冷却效率的求解方法.动力工程学报, 2023, 43(12), pp. 1577-1584
6. 戴思明, 李佳宁, 方一之, 马海腾*. 超声速流动中的离散孔气膜冷却实验研究. 第七届中国空天动力联合大会（成都专场）, 四川成都, 2023

2022年
7. Ma, H.*, Zeng, W., Dai, S., Jiang, H., 2022, "Sensitivity of Adiabatic Cooling Effectiveness to Mainstream and Coolant Temperatures in Transonic Flow Over an Idealized Blade Tip Model", ASME Journal of Turbomachinery, Vol. 144, No. 11, pp. 111013 (12 pages)
8. Ma, H.*, Zeng, W., Jiang, H., Hong, J., 2022, "Impact of Cooling Injection on Shock Wave over a Flat Tip in High Pressure Turbine", ASME Journal of Turbomachinery, Vol. 144, No. 1, pp. 011012 (13 pages)
9. Ma, H.*, He, L., Yu, G., Yu, Z., 2022, “Natural Convection Heat Transfer and Fluid Flow in a Thermal Chimney With Multiple Horizontally-aligned Cylinders”, International Journal of Heat and Mass Transfer, Vol. 183, Part C, pp. 122239 (13 pages)
10. Ma H.*, Zeng W., Dai S., Jiang H., 2022, "Sensitivity of Adiabatic Cooling Effectiveness to Mainstream and Coolant Temperatures in Transonic Flow Over an Idealized Blade Tip Model," ASME Turbo Expo Conference, Rotterdam, The Netherlands, Paper No. GT2022-82778
11. Ma H., Liu Y., Lai Y., Ouyang H.*, Ning J., Jiang X., Xu Q., 2022, "Magnetic Resonance Velocimetry of A Turbine Blade With Engine Representative Internal and Film Cooling Structures," ASME Turbo Expo Conference, Rotterdam, The Netherlands, Paper No. GT2022-82849
12. 曾伟, 马海腾*. 炮风洞有效测试时间的影响机制. 第十二届全国流体力学学术会议, 线上/陕西西安, 2022, doi: 10.26914/c.cnkihy.2022.068336
13. 曾伟, 马海腾*. 炮风洞有效测试时间的影响机制. 第二十届激波与激波管学术会议, 线上/合肥, 2022.

2021年
14. Ma, H.*, and He, L., 2021, “Large Eddy Simulation of Natural Convection Heat Transfer and Fluid Flow around a Horizontal Cylinder,” International Journal of Thermal Sciences, Vol. 162, pp. 106789 (15 pages).

2020年
15. Lu, S.*, Ma, H., Zhang, Q., Teng, J., 2020, "Cutback Squealer Tip Trailing Edge Cooling Performance," International Journal of Heat and Mass Transfer, Vol. 154, pp. 119632 (15 pages).

2019年
16. 王维杰,卢少鹏,马海腾,张强,滕金芳,余文胜.高压涡轮尾切凹槽叶尖冷却换热特性[J].航空动力学报,2019,34(10):2131-2139.
17. Ma, H.*, He, L., Rane, S., 2019, “Heat Transfer-Fluid Flow Interaction in Natural Convection around Heated Cylinder and Its Thermal Chimney Effect,” International Conference on Innovative Applied Energy, Oxford, UK
18. Rane, S., He, L., Ma, H., 2019, "CFD modelling and analysis of Two-Phase Geothermal Energy Turbine in Project Combi-Gen," International Conference on Innovative Applied Energy, Oxford, UK
19. Burnside, N., Rane, S., Yu, G., Ma, H., Montcoudiol, N., Li, W., Teklemariam, E., Boyce, A., He, L., Yu, Z., 2019, "Geothermally Sourced Combined Power and Freshwater Generation for Eastern Africa," European Geothermal Congress, Den Haag, Netherlands

2018年及以前
20. Ma, H., Zhang, Q.*, He, L., Wang, Z., and Wang, L., 2017, “Cooling Injection Effect on a Transonic Squealer Tip - Part 1: Experimental Heat Transfer Results and CFD Validation,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 139, No. 5, pp. 052506 (9 pages).
21. Ma, H., Zhang, Q.*, He, L., Wang, Z., and Wang, L., 2017, “Cooling Injection Effect on a Transonic Squealer Tip - Part 2: Analysis of Aerothermal Interaction Physics,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 139, No. 5, pp. 052507 (9 pages).
22. Ma, H., Wang, Z., Wang, L., Zhang Q.*, Yang Z., and Bao Y., 2016, "Ramp Heating in High-Speed Transient Thermal Measurement with Reduced Uncertainty," AIAA Journal of Propulsion and Power, Vol. 32, No. 5, pp. 1190-1198.
23. Zhong, F., Zhou, C.*, Ma, H., and Zhang, Q., 2017, “Heat Transfer on Winglet Tips in a Transonic Turbine Cascade,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 139, No. 1, pp. 012605 (11 pages).
24. Ma, H., Zhang, Q.*, He, L., Wang, Z., and Wang, L., 2016, “Cooling Injection Effect on a Transonic Squealer Tip - Part 1: Experimental Heat Transfer Results and CFD Validation,” ASME Turbo Expo Conference, Seoul, South Korea, Paper No. GT2016-57579.
25. Ma, H., Zhang, Q.*, He, L., Wang, Z., and Wang, L, 2016, “Cooling Injection Effect on a Transonic Squealer Tip - Part 2: Analysis of Aerothermal Interaction Physics,” ASME Turbo Expo Best Paper Award, Seoul, South Korea, Paper No. GT2016-57587.
26. Ma, H., Wang, Z., Wang, L., Zhang, Q.*, Yang, Z., and Bao, Y., 2015, “Ramp Heating in High-Speed Transient Thermal Measurement with Reduced Uncertainty,” ASME Turbo Expo Conference, Montreal, Canada, Paper No. GT2015-43012.
27. Zhu, D., Lu, S., Ma, H., Zhang, Q., Teng, J., 2017, “Rotating Effect on Transonic Squealer Tip Cooling Performance,” ASME Turbo Expo Conference, Charlotte, US, Paper No. GT2017-64293.
28. Zhong, F., Zhou, C.*, Ma, H., and Zhang, Q., 2016, “Heat Transfer on Winglet Tips in a Transonic Turbine Cascade,” ASME Turbo Expo Conferenc, Seoul, South Korea, Paper No. GT2016-56804
29. Zhang, X., Yang, Z., Tian, S., and Ma, H., 2015, “Numerical Study of the Film Cooling With Discrete Hole Arrangement on a Cutback Squealer Turbine Blade Tip,” ASME Turbo Expo Conference, Montreal, Canada, Paper No. GT2015-43877