郑新前,清华大学长聘教授、博士生导师,美国普林斯顿大学访问学者,国家基础加强计划首席科学家,国家高层次人才,科技部中青年科技创新领军人才,中国青年科技奖、国家科技进步二等奖、中国内燃机学会突出贡献奖获得者,美国航空航天学会副会士,国际期刊ASMEJournal of Engineering for Gas Turbines and Power和AerospaceScience and Technology副主编。长期从事航空、车辆、船舶等领域的能源与动力研究,主持国家、GF、国际等各类项目70余项,发表学术论文180余篇,SCI论文130余篇,授权国内国际发明专利50余项。
教育背景
2000年-2006年,
北京航空航天大学,
能源与动力工程学院
1996年-2000年,
西北工业大学,能源与动力工程学院
工作履历
2023 - , 清华大学车辆与运载学院,长聘教授
2019-2023,清华大学车辆与运载学院/航空发动机研究院,长聘教授
2018-2019,清华大学车辆与运载学院/航天航空学院,长聘教授
2017-2018,清华大学车辆与运载学院/航天航空学院,长聘副教授
2010-2016,清华大学汽车工程系,副研究员
2008-2010,清华大学汽车工程系,助理研究员
2006-2008,清华大学汽车工程系,博士后
人才培养
先后讲授本科生和研究生课程《流体力学》、《内燃机增压与增压技术》、《计算流体力学》、《航空发动机原理》、《航空发动机技术前沿》等课程,获清华大学“青年教师教学优秀奖”。培养博士生近30人、硕士生近10人,指导本科毕设及SRT近60人,培养指导的学生多人次获得清华大学优秀博士论文、清华大学优秀硕士论文、清华大学优秀本科论文、北京市/清华大学优秀博士毕业生、北京市/清华大学优秀硕士毕业生等荣誉。
研究领域
长期从事航空、车辆、船舶等领域的能源与动力研究,先后主持国家、GF、国际等各类项目70余项。主要研究包括:自适应变循环发动机,临近空间长航时无人机(氢能)动力,高速智能蜂群动力,燃料电池涡轮增压,活塞发动机涡轮增压,新能源汽车综合热管理,人工智能大数据中心综合热管理,航空动力综合热管理等。
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。
获得荣誉
(1) 国家高层次人才
(2) 中国青年科技奖
(3) 国家科技进步二等奖
(4) 国防科技进步一等奖
(5) 中国机械工业科学技术一等奖
(6) 美国航空航天学会副会士
(7) 中国内燃机学会突出贡献奖
(8) 美国机械工程师协会最佳论文奖
(9) 英国机械工程师协会最佳论文奖
(10) 清华大学“学术新人奖”
(11) 清华大学“青年教师教学优秀奖”
(12) 教育部霍英东基金
(13) 全国优秀博士学位论文
学术成果
共发表(含录用)论文180余篇,其中SCI收录130篇,授权国内国际发明专利50余项。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等国际期刊发表论文40余篇。授权发明专利美国4项、日本5项、中国18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:)
Energy
[21] 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
[22] 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:)
[23] 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)
[24] 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)
[25] 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
[26] 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)
[27] 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)
[28] 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
[29] 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.
[30] 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)
[31] 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)
[32] 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
[33] 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:)
[34] 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:)
[35] 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)
[36] 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)
[37] 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)
[38] 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)
[39] 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)
[40] 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
[41] 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.
[42] 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:)
[43] ZHENGXinqian*, 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)
[44] 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)
[45] 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)
[46] 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)
[47] 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)
[48] 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
[49] 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: )
[50] 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)
[51] 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)
[52] 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)
[53] 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)
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)