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，国家“”科技创新领军人才，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，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：清华大学李兆基科技大楼A339
网址：http://www.turbo.dae.tsinghua.edu.cn/index.php





个人主页


教育背景
工作履历
研究领域
研究概况
学术兼职
荣誉与奖励
学术成果
2000.09-2006.03，北京航空航天大学，能源与动力工程学院
1996.09-2000.06，西北工业大学，能源与动力工程学院


2018.12-至今， 清华大学航天航空学院（双聘），长聘教授/博导
2018.12-至今， 清华大学汽车工程系，长聘教授/博导
2016.12-2018.11，清华大学汽车工程系，长聘副教授/博导
2013.09-2016.11，清华大学汽车工程系，副研究员/博导
2010.12-2013.08，清华大学汽车工程系，副研究员/硕导
2008.04-2010.11，清华大学汽车工程系，助理研究员/硕导
2006.04-2008.03，清华大学汽车工程系，博士后
2011.07-2012.07，普林斯顿大学，访问

所授课程
《计算流体力学》
《发动机涡轮增压技术》


先进航空涡轮发动机（涡轴、涡桨、涡喷、涡扇）流动与叶轮机械技术
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


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。
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



(1)入选国家“”科技创新领军人才（2019年）
(2)入选创新人才推进计划中青年科技创新领军人才（2018年）
(3)入选美国航空航天学会AIAA Associate Fellow（2018年，中国3人）
(4)荣获首届中国内燃机工业杰出科技创新奖（2018年）
(5)荣获中国内燃机学会突出贡献奖（2017年，全国2人）
(6)荣获中国青年科技奖（2016年）
(7)荣获清华大学“青年教师教学优秀奖”（2015年，清华10人）
(8)荣获清华大学“学术新人奖”（2015年，清华10人）
(9)荣获国防科技进步三等奖（2015年）
(10)荣获中国内燃机学会史绍熙人才奖（2014年，全国3人）
(11)荣获美国机械工程师协会最佳论文奖（2013年）
(12)荣获国家科技进步二等奖（2013年）
(13)荣获国防科技进步一等奖（2013年）
(14)入选教育部“新世纪优秀人才”支持计划（2013年）
(15)荣获茅以升北京青年科技奖（2013年，北京15人）
(16)荣获英国机械工程师协会最佳论文奖（2011年）
(17)荣获山东省科技进步二等奖（2011年）
(18)荣获国防技术发明三等奖（2011年）
(19)荣获教育部霍英东基金（2010年）
(20)荣获全国优秀博士学位论文（2008年）



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: 20**9)
[2]LI Zhihui, ZHENG Xinqian*, “Review of Design Optimization Methods for Turbomachinery Aerodynamics,” Progress in Aerospace Sciences, 2017, 93: 1-23. (SCI: FI8QC ; EI: 20**1)

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: 20**3)
[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: 20**8)
[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: 947)
[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: 946)
[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: 20**6)
[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:397)
[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: 141)
[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: 19)

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: 20**9)
[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:20**3)
[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: 20**2)
[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: 20**3)
[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: 20**5)

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: 20**3)

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: 20**5)

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: 20**7)
[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: 20**5)
[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: 20**5)

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:20**7)
[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: 20**2)
[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:20**2)

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: 20**7)
[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: 20**9)
[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: 521; 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: 10.1177/7926. (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: 10.1177/6281. (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: 20**4)
[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: 20**1)
[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: 20**7)
[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: 20**3)
[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: 20**2)
[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: 920)

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: 10.1177/4884. (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: 10.1177/0418. (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: 20**1)
[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: 20**3)
[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: 20**8)
[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: 20**4)

[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: 20**1)

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: 20**8)
[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: 20**8)
[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: 20**7)
[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: 776)
[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: 379)