职称:教授

E-mail address👩🏻‍🚀:zhengxq@tsinghua.edu.cn

个人简介

郑新前,杏福娱乐长聘教授、博士生导师🤾🏽‍♂️,美国普林斯顿大学访问学者🙅🏿‍♂️𓀕,中国青年科技奖、国家科技进步奖获得者,美国航空航天学会涡轮发动机专业委员会委员,美国航空航天学会AIAA Associate Fellow,国际顶尖权威期刊ASME Journal of Engineering for Gas Turbines and Power🥈🧖🏼、Aerospace Science and Technology副主编🤾🏻‍♀️。面向国家重大需求和国际学术前沿𓀛🛌,长期从事航空发动机和涡轮增压内燃机研究,先后主持国家🦹🏻‍♂️、国防、国际等课题40余项,发表学术论文120余篇(SCI论文70余篇),授权发明专利29项(美国4项、日本5项、中国20项)。

邮箱:zhengxq@tsinghua.edu.cn

地址🦵🏿🔂:杏福娱乐李兆基科技大楼A339

网址:http://www.turbo.dae.tsinghua.edu.cn/index.php

所授课程

《计算流体力学》

《发动机涡轮增压技术》

教育背景

2000.09-2006.03✹,北京航空航天大学,能源与动力工程杏福

1996.09-2000.06🍂,西北工业大学,动力与能源杏福

工作履历

2018.12-至今, 杏福(双聘),长聘教授/博导

2018.12-至今, 杏福娱乐汽车工程系,长聘教授/博导

2016.12-2018.11,杏福娱乐汽车工程系♥️,长聘副教授/博导

2013.09-2016.11🏊🏿,杏福娱乐汽车工程系,副研究员/博导

2010.12-2013.08,杏福娱乐汽车工程系💂🏼‍♀️,副研究员/硕导

2008.04-2010.11👼🏿,杏福娱乐汽车工程系,助理研究员/硕导

2006.04-2008.03,杏福娱乐汽车工程系,博士后

2011.07-2012.07🧕🏻🫀,普林斯顿大学,访问学者

学术兼职

美国航空航天学会涡轮发动机专业委员会委员

ASME Journal of Engineering for Gas Turbines and Power 副主编

Aerospace Science and Technology副主编

International Journal of Fluid Machinery and Systems副主编

Applied Sciences 客座主编

研究领域

先进航空涡轮发动机(涡轴👨‍👨‍👧🔒、涡桨🪜、涡喷、涡扇)与叶轮机械技术

先进节能内燃机(汽油🔑、柴油✊🏿💁🏻、氢能)与涡轮增压技术

先进车用/航空发动机混合动力技术

新能源燃料电池涡轮增压技术

新能源车用微型燃气轮机增程器技术

研究概况

主持国家“两机”重大专项、国家自然科学基金、科技部、教育部😣、总装、国防科工局🧑‍🦼🟰、中国航空发动机集团、中国航天科工集团💇🏽‍♂️、中国第一汽车集团、IHI、博马科技等国家、国防🤷🏿、国际各类课题40余项🧑🏿‍🎤。

奖励与荣誉

入选美国航空航天学会AIAA Associate Fellow(2018年,中国3人)

荣获首届中国内燃机工业杰出科技创新奖(2018年)

荣获中国内燃机学会突出贡献奖(2017年🏄🏽,全国2人)

荣获中国青年科技奖(2016年)

荣获杏福娱乐“青年教师教学优秀奖”(2015年🪭,杏福10人)

荣获杏福娱乐“学术新人奖”(2015年🏉,杏福10人)

荣获国防科技进步三等奖(2015年)

荣获中国内燃机学会史绍熙人才奖(2014年,全国3人)

荣获美国机械工程师协会最佳论文奖(2013年)

荣获国家科技进步二等奖(2013年)

荣获国防科技进步一等奖(2013年)

入选教育部“新世纪优秀人才”支持计划(2013年)

荣获茅以升北京青年科技奖(2013年,北京15人)

荣获英国机械工程师协会最佳论文奖(2011年)

荣获山东省科技进步二等奖(2011年)

荣获国防技术发明三等奖(2011年)

荣获教育部霍英东基金(2010年)

荣获全国优秀博士学位论文(2008年)

学术成果

共发表(含录用)论文120余篇📭,其中SCI收录70余篇🫅🏿,EI收录110余篇🏀。在ASME Journal of Turbomachinery🤾🏼‍♂️、AIAA Journal of Propulsion and Power、Progress in Aerospace Sciences👰🏽、Aerospace Science and Technology、Energy👨‍👧‍👧、Applied Energy、Experimental Thermal and Fluid Sciences💂🏽‍♂️📕、Applied Thermal Engineering👦🏽、International Journal of Heat and Fluid Flow等国际权威期刊发表论文40余篇😎。授权发明专利29项👨‍🔬😷,其中美国4项、日本5项、中国20项。代表性论文列表如下(*为通讯作者)💇🏼:

Progress in Aerospace Sciences

[1] ZHENG Xinqian*, LI Zhihui, “Blade-end Treatment to Improve the Performance of Axial Compressors: An Overview,” Progress in Aerospace Sciences, 2017, 88: 1–14. (SCI: EI8PY; EI: 20165003110729)

[2] LI Zhihui, ZHENG Xinqian*, “Review of Design Optimization Methods for Turbomachinery Aerodynamics,” Progress in Aerospace Sciences, 2017, 93: 1-23. (SCI: FI8QC ; EI: 20172903947521)

ASME Journal of Turbomachinery

[3] ZHENG Xinqian*, SUN Zhenzhong, KAWAKUBO Tomoki, TAMAKI Hideaki, “Stability Improvement of a Turbocharger Centrifugal Compressor by Non-Axisymmetric Vaned Diffuser,” Journal of Turbomachinery-Transactions of the ASME, 2018, 140 (4): 041007-1~13. (SCI: ; EI:)

[4] ZHENG Xinqian*, HUANG Qiangqiang, LIU Anxiong, “Loss Mechanisms and Flow Control for Improved Efficiency of a Centrifugal Compressor at High Inlet Prewhirl,” Journal of Turbomachinery-Transactions of the ASME, 2016, 138: 101011-1~11. (SCI: BF1AF; EI: 20162402492753)

[5] ZHENG Xinqian*, Liu Anxiong, “Phenomenon and Mechanism of Two-Regime-Surge in a Centrifugal Compressor,” Journal of Turbomachinery-Transactions of the ASME, 2015, 137 (8): 081007-1~7. (SCI: CL3FI; EI: 20152901032948)

[6] ZHENG Xinqian*, ZHANG Yangjun, YANG Mingyang, BAMBA Takahiro, TAMAKI Hideaki, “Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control——Part II: Non-Axisymmetric Self Recirculation Casing Treatment,” Journal of Turbomachinery-Transactions of the ASME, 2013, 135 (2): 021007-1~8. (SCI: 094KB; EI: 20124515648947)

[7] YANG Mingyang, ZHENG Xinqian*, ZHANG Yangjun, BAMBA Takahiro, TAMAKI Hideaki, HUENTELER Joern, LI Zhigang, “Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control——Part I: Non-Axisymmetric Flow in Centrifugal Compressor,” Journal of Turbomachinery-Transactions of the ASME, 2013, 135 (2): 021006-1~9. (SCI: 094KB; EI: 20124515648946)

[8] TAMAKI Hideaki*, ZHENG Xinqian, ZHANG Yangjun, “Experimental Investigation of High Pressure Ratio Centrifugal Compressor with Axisymmetric and Nonaxisymmetric Recirculation Device,” Journal of Turbomachinery-Transactions of the ASME, 2013, 135 (3): 031023-1~12. (SCI: 239KD; EI: 20133316600816)

[9] ZHENG Xinqian*, ZHANG Yangjun, XING Weidong, ZHANG Junyue, “Separation Control of Axial Compressor Cascade by Fluidic-Based Excitations,” Journal of Turbomachinery-Transactions of the ASME, 2011, 133 (4): 041016-1~7. (SCI: 755SH; EI:20111713934397)

[10] ZHENG Xinqian*, ZHOU Sheng, LU Yajun, HOU Anping, LI Qiushi, “Flow Control of Annular Compressor Cascade by Synthetic Jets,” Journal of Turbomachinery-Transactions of the ASME, 2008, 130 (2): 021018-1~7. (SCI: 279UP; EI: 20083111418141)

[11] ZHENG Xinqian*, ZHOU Xiaobo, ZHOU Sheng, “Investigation on a Type of Flow Control to Weaken Unsteady Separated Flows by Unsteady Excitation in Axial Flow Compressors,” Journal of Turbomachinery-Transactions of the ASME, 2005, 127 (3): 489–496. (SCI: 953KC; EI: 2005359327819)

ASME Journal of Engineering for Gas Turbines and Power

[12] ZHANG Meijie, ZHENG Xinqian*, HUANG Qiangqiang, SUN Zhenzhong, “A Novel 1D-3D Coupled Method to Predict Surge Boundary of Centrifugal Compressors,” ASME Journal of Engineering for Gas Turbines and Power, Accepted. (SCI:;EI:)

[13] SHU Mengying, YANG Mingyang*, DENG Kangyao, ZHENG Xinqian, MARTINEZ-BOTAS Ricardo, “Performance Analysis of a Centrifugal Compressor Based on Circumferential Flow Distortion Induced by Volute,” ASME Journal of Engineering for Gas Turbines and Power, 2018, 140: 122603-1~11. (SCI:;EI:)

AIAA Journal of Propulsion and Power

[14] ZHENG Xinqian*, YANG Heli, “End-Wall Boundary Layers and Blockages of Multistage Axial Compressors Under Different Conditions,” AIAA Journal of Propulsion and Power, 2017, 33 (4): 908-916. (SCI: EY9UP; EI: 20172603859149)

[15] HUANG Qiangqiang, ZHENG Xinqian*, “Potential of Variable Geometry Method on Compressor Range Extension for Turbocharged Engines,” AIAA Journal of Propulsion and Power, 2017, 33 (5): 1197-1206. (SCI: FE6JA, EI:20173504098403)

[16] HE Xiao, ZHENG Xinqian*, “The Mechanisms of Lean on the Performance of Transonic Centrifugal Compressor Impellers,” AIAA Journal of Propulsion and Power, 2016, 32 (5): 1220-1229. (SCI: DW2MH; EI: 20163502763102)

[17] YANG Mingyang*, MARTINEZ-BOTAS Ricardo, ZHANG Yangjun, ZHENG Xinqian, “Effect of Self-Recirculation-Casing Treatment on High Pressure Ratio Centrifugal Compressor,” AIAA Journal of Propulsion and Power, 2016, 32 (3): 602-610. (SCI: DM9GH; EI: 20162102420993)

[18] ZHENG Xinqian*, LIU Anxiong, “Experimental Investigation of Surge and Stall in a High-Speed Centrifugal Compressor,” AIAA Journal of Propulsion and Power, 2015, 31 (3): 815-825. (SCI: CQ8ES; EI: 20152000847455)

Aerospace Science and Technology

[19] HE Xiao, ZHENG Xinqian*, “Roles and Mechanisms of Casing Treatment on Different Scales of Flow Instability in Centrifugal Compressors,” Aerospace Science and Technology, 2019, 84: 734-746. (SCI:;EI:)

[20] SUN Zhenzhong, ZOU Wangzhi, ZHENG Xinqian*, “Instability Detection of Centrifugal Compressors by Means of Acoustic Measurements” Aerospace Science and Technology, 2018, 82-83: 628-635. (SCI:;EI:)

Applied Energy

[21] ZHU Dengting, ZHENG Xinqian*, “Fuel Consumption and Emission Characteristics in Asymmetric Twin-Scroll Turbocharged Diesel Engine with Two Exhaust Gas Recirculation Circuits, Applied Energy, Accepted. (SCI: ; EI:)

[22] ZHU Dengting, ZHENG Xinqian*, “A New Asymmetric Twin-Scroll Turbine with Two Wastegates for Energy Improvements in Diesel Engines,” Applied Energy, 2018, 223: 263–272. (SCI: GH7RA; EI: 20181805131813)

Energy

[23] ZHU Dengting, ZHENG Xinqian*, “Asymmetric Twin-Scroll Turbocharging in Diesel Engines for Energy and Emission Improvement,” Energy, 2017, 141: 702-714. (SCI: FX8IM; EI: 20174104243415)

Experimental Thermal and Fluid Science

[24] ZHANG Meijie, ZHENG Xinqian*, SUN Zhenzhong, “Experimental Investigation of the Flow Instability of a Compression System with an Upstream Plenum,” Experimental Thermal and Fluid Science, 2019, 102: 406-420. (SCI:;EI:)

[25] HE Xiao, ZHENG Xinqian*, “Flow Instability Evolution in High Pressure Ratio Centrifugal Compressor with Vaned Diffuser,” Experimental Thermal and Fluid Science, 2018, 98, 719-730. (SCI: GQ6SL ; EI: 20183005584577)

[26] ZHENG Xinqian*, SUN Zhenzhong, KAWAKUBO Tomoki, TAMAKI Hideak, “Experimental Investigation of Surge and Stall in a Turbocharger Centrifugal Compressor with a Vaned Diffuser,” Experimental Thermal and Fluid Science, 2017, 82: 493-506. (SCI: EI8PI; EI: 20165203194855)

[27] LIU Anxiong, ZHENG Xinqian*, “Methods of Surge Point Judgment for Compressor Experiments”, Experimental Thermal and Fluid Science, 2013, 51: 204-213. (SCI: 249HH; EI: 20134016808435)

Applied Thermal Engineering

[28] SUN Zhenzhong, ZHENG Xinqian*, KAWAKUBO Tomoki, “Experimental Investigation of Instability Inducement and Mechanism of Centrifugal Compressors with Vaned Diffuser,” Applied thermal Engineering, 2018, 133: 464-471. (SCI: ; EI:20180604768787)

[29] ZHANG Meijie, ZHENG Xinqian*, “Criteria for the Matching of Inlet and Outlet Distortions in Centrifugal Compressors,” Applied Thermal Engineering, 2018, 131: 933–946. (SCI:FU9JZ ; EI: 20175304592092)

[30] MOSTAFA Moosania, ZHENG Xinqian*, “Effect of Internal Heat leakage on the Performance of a High Pressure Ratio Centrifugal Compressor,” Applied Thermal Engineering, 2017, 111: 317-324. (SCI:EH6PU;EI:20163902856012)

IMechE Part A: Journal of Power and Energy

[31] ZHU Dengting, ZHENG Xinqian*, “Strategy on Performance Improvement of Inverse Brayton Cycle System for Energy Recovery in Turbocharged Diesel Engines,” IMechE Part A: Journal of Power and Energy, 2019, Accept.

[32] ZHENG Xinqian*, JIN Lei, TAMAKI Hideaki, “Influence of Volute-Induced Distortion on the Performance of a High-pressure-ratio Centrifugal Compressor with a Vaneless Diffuser for Turbocharger Applications,” IMechE Part A: Journal of Power and Energy, 2014, 228 (4): 440-450. (SCI:AG8GH; EI: 20141917699337)

[33] YANG Dong, ZHENG Xinqian, LI Qiushi*, “An 11-Stage Axial Compressor Performance Simulation Considering the Change of Tip Clearance in Different Operating Conditions,” IMechE Part A: Journal of Power and Energy, 2014, 228 (6): 614-625. (SCI: AM8YT; EI: 20143118009029)

[34] ZHENG Xinqian*, HUENTELE Joern, YANG Mingyang, ZHANG Yangjun, BAMBA Takahiro, “Influence of the Volute on the Flow in a Centrifugal Compressor of a High-pressure Ratio Turbocharger,” IMechE Part A: Journal of Power and Energy, 2010, 224 (A8): 1157-1169. (SCI:689PP; EI: 20112013991521; SAGE Best Paper Award)

IMechE Part D: Journal of Automobile Engineering

[35] WANG Aolin, ZHENG Xinqian*, “Design Criterion for Asymmetric Twin-Entry Radial Turbine for Efficiency under Steady and Pulsating Inlet Conditions,” IMechE Part D: Journal of Automobile Engineering, 2018, Online, DOI: 10.1177/0954407018757926. (SCI: ; EI:)

[36] SUN Zhenzhong, ZHENG Xinqian*, LINGHU Zelin, KAWAKUBO Tomoki, TAMAKI Hideaki, WANG Baotong, “Influence of Volute Design on Flow Field Distortion and Flow Stability of Turbocharger Centrifugal Compressors,” IMechE Part D: Journal of Automobile Engineering, 2018, Online, DOI: 10.1177/0954407017746281. (SCI: ; EI:)

[37] ZHENG Xinqian*, LIU Anxiong, SUN Zhenzhong, “Investigation of the Instability Mechanisms in a Turbocharger Centrifugal Compressor with a Vaneless Diffuser by Means of Unsteady Simulations,” IMechE Part D: Journal of Automobile Engineering, 2017, 231 (11): 1558-1567. (SCI: FF1CX; EI: 20173604117864)

[38] HUANG Qiangqiang, ZHENG Xinqian*, “Potential of Variable Diffuser Vanes For Extending the Operating Range of Compressors and for Improving the Torque Performance of Turbocharged Engines,” IMechE Part D: Journal of Automobile Engineering, 2017, 231 (4): 555-566. (SCI: EP2KK; EI: 20171003422011)

[39] MIRZAEE Saeed, ZHENG Xinqian*, LIN Yun, “Improvement in the Stability of a Turbocharger Centrifugal Compressor by Tip Leakage Control,” IMechE Part D: Journal of Automobile Engineering, 2017, 231 (5): 700-714. (SCI: ES7CQ; EI: 20171903643577)

[40] ZHENG Xinqian*, HUANG Qiangqiang, “Potential of the Range Extension of Compressors with a Variable inlet Prewhirl for Automotive Turbocharged Engines with an Ultra-High-Power Density,” IMechE Part D: Journal of Automobile Engineering, 2015, 229 (14): 1959-1968. (SCI: CW7IX; EI: 20154801604013)

[41] ZHENG Xinqian*, LAN Chuanjie, “Improvement in the Performance of a High-Pressure-Ratio Turbocharger Centrifugal Compressor by Blade Bowing and Self-recirculation Casing Treatment,” IMechE Part D: Journal of Automobile Engineering, 2014, 228 (1): 73-84. (SCI:293HK; EI: 20140517259632)

[42] ZHUGE Weilin, ZHANG Yangjun*, ZHENG Xinqian, YANG Mingyang, HE Yongshen, “Development of an Advanced Turbocharger Simulation Method for Cycle Simulation of Turbocharged Internal Combustion Engines,” IMechE Part D: Journal of Automobile Engineering, 2009, 223 (5): 661-672. (SCI: 449VQ; EI: 20092212102920)

IMechE Part G: Journal of Aerospace Engineering

[43] ZOU Wangzhi, ZHANG Wenchao, NIU Zitian, ZHENG Xinqian, “Roles of Vanes in Diffuser on Stability of Centrifugal Compressor,” IMechE Part G: Journal of Aerospace Engineering, 2019, Accept.

[44] YANG Heli, ZHENG Xinqian*, “Investigation of Endwall Treatment and Shock Control in a Five-Stage Axial Compressor,” IMechE Part G: Journal of Aerospace Engineering, 2018, Online, DOI: 10.1177/0954410017734884. (SCI: ; EI:)

[45] ZHENG Xinqian*, LIN Yun, SUN Zhenzhong, “Effects of Volute’s Asymmetry on the Performance of a Turbocharger Centrifugal Compressor,” IMechE Part G: Journal of Aerospace Engineering, 2018, Online, DOI: 10.1177/0954410016670418. (SCI; EI)

[46] HE Xiao, ZHENG Xinqian*, “Performance Improvement of Transonic Centrifugal Compressors by Optimization of Complex Three-Dimensional Features,” IMechE Part G: Journal of Aerospace Engineering, 2017, 231 (14): 2723-2738. (SCI: FM7MQ; EI: 20174704434331)

[47] ZHENG Xinqian*, DING Chuang, ZHANG Yangjun, “Influence of Different Loads on the Stresses of Multistage Axial Compressor Rotors,” IMechE Part G: Journal of Aerospace Engineering, 2017, 231 (5): 787-798. (SCI: ES4HI; EI: 20171903643373)

[48] MOSTAFA Moosania, ZHENG Xinqian*, “Performance Improvement of a High Pressure Ratio Centrifugal Compressor by Integrated Cooling,” IMechE Part G: Journal of Aerospace Engineering, 2016, 230 (12): 2233–2240. (SCI: DV5LV; EI: 20163702804198)

[49] LI Zhihui, ZHENG Xinqian, LIU Yangming*, LI Qiushi, JI Baohua, “The Effect of End Wall Boundary Layer on Matching and Corresponding Flow Control Technique for Multistage Axial Compressor,” IMechE Part G: Journal of Aerospace Engineering, 2016, 230 (12): 2179–2194. (SCI: DV5LV; EI: 20163702804194)

[50] LU Hanan, ZHENG Xinqian, LI Qiushi*, “A Combinatorial Optimization Design Method Applied to S-Shaped Compressor Transition Duct Design,” IMechE Part G: Journal of Aerospace Engineering, 2014, 228 (10): 1749-1758. (SCI: AM8NB; EI: 20142917956491)

Sci China

[51] LINGHU Zelin, ZHAO Chenjia, YANG Heng, ZHENG Xinqian*, “Beetle Wing Folding Facilitated by Micro-Protrusions on the Body Surface: a Case of Allomyrina Dichotoma,” Science Bulletin, 2015, 60 (16): 1457-1460. (SCI: CQ4CC; EI: )

[52] ZHENG Xinqian*, LAN ChuanJie, “Effects of Blade Bowing on the Performance of a High Pressure-Ratio Turbocharger Centrifugal Compressor with Self-recirculation Casing Treatment,” Sci China Ser E-Tech Sci, 2013, 56 (10): 2531-2539. (SCI: 227PL; EI: 20134216867928)

[53] ZHENG Xinqian*, LIN Yun, GAN Binlin, ZHUGE Weilin, ZHANG Yangjun, “Effects of Reynolds Number on the Performance of a High Pressure-Ratio Turbocharger Compressor,” Sci China Ser E-Tech Sci, 2013, 56 (6): 1361-1369. (SCI: 168WR; EI: 20132816483688)

[54] ZHENG Xinqian*, JIN Lei, TAMAKI Hideaki, “Influence of Volute Distortion on the Performance of Turbocharger Centrifugal Compressor with Vane Diffuser”, Sci China Ser E-Tech Sci, 2013, 56 (11): 2778-27869. (SCI: 245JL; EI: 20134817033077)

[55] LIN Yun, ZHENG Xinqian*, JIN Lei, TAMAKI Hideaki, KAWAKUBO Tomoki, “A Novel Experimental Method to Evaluate the Impact of the Volute’S Asymmetry on the Performance of a High Pressure Ratio Turbocharger Compressor,” Sci China Ser E-Tech Sci, 2012, 55 (6): 1695-1700. (SCI: 943KV; EI: 20122615154776)

[56] ZHENG Xinqian*, ZHANG Yangjun, YANG Mingyang, “Research and Development on Transonic Compressor of High Pressure Ratio Turbocharger for Vehicle Internal Combustion Engines,” Sci China Ser E-Tech Sci, 2010, 53 (7): 1817-1823. (SCI: 621SZ; EI: 20103313151379)

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