电话:010-62796167
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E-mail:qcxbgs@tsinghua.edu.cn
pg电子游戏官网官方网站长聘教授、博士生导师,美国普林斯顿大学访问学者,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:pg电子游戏官网官方网站李兆基科技大楼A339
网址:http://www.turbo.dae.tsinghua.edu.cn/index.php
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, pg电子游戏官网官方网站航天航空学院(双聘),长聘教授/博导
2018.12-至今,
pg电子游戏官网官方网站汽车工程系,长聘教授/博导
2016.12-2018.11,pg电子游戏官网官方网站汽车工程系,长聘副教授/博导
2013.09-2016.11,pg电子游戏官网官方网站汽车工程系,副研究员/博导
2010.12-2013.08,pg电子游戏官网官方网站汽车工程系,副研究员/硕导
2008.04-2010.11,pg电子游戏官网官方网站汽车工程系,助理研究员/硕导
2006.04-2008.03,pg电子游戏官网官方网站汽车工程系,博士后
2011.07-2012.07,普林斯顿大学,访问学者
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
主持国家自然科学基金、科技部、教育部、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)入选美国航空航天学会AIAA
Associate
Fellow(2018年,中国3人)
(2)荣获首届中国内燃机工业杰出科技创新奖(2018年)
(3)荣获中国内燃机学会突出贡献奖(2017年,全国2人)
(4)荣获中国青年科技奖(2016年)
(5)荣获pg电子游戏官网官方网站“青年教师教学优秀奖”(2015年,清华10人)
(6)荣获pg电子游戏官网官方网站“学术新人奖”(2015年,清华10人)
(7)荣获中国内燃机学会史绍熙人才奖(2014年,全国3人)
(8)荣获美国机械工程师协会最佳论文奖(2013年)
(9)荣获国家科技进步二等奖(2013年)
(10)入选教育部“新世纪优秀人才”支持计划(2013年)
(11)荣获茅以升北京青年科技奖(2013年,北京15人)
(12)荣获英国机械工程师协会最佳论文奖(2011年)
(13)荣获山东省科技进步二等奖(2011年)
(14)荣获教育部霍英东基金(2010年)
(15)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:
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)