鄭新前，清華大學長聘教授、博士生導師，美國普林斯頓大學訪問學者，國家“萬人計畫”科技創新領軍人才，中國青年科技獎、國家科技進步獎獲得者，美國航空航天學會渦輪發動機專業委員會委員，美國航空航天學會AIAA Associate Fellow，國際頂尖權威期刊ASME Journal of Engineering for Gas Turbines and Power、Aerospace Science and Technology副主編。面向國家重大需求和國際學術前沿，長期從事航空發動機和渦輪增壓內燃機研究，先後主持國家、國防、國際等課題40餘項，發表學術論文120餘篇（SCI論文70餘篇），授權發明專利29項（美國4項、日本5項、中國20項）。
基本介紹
- 中文名：鄭新前
- 國籍：中國
- 民族：漢
- 出生地：四川內江
- 職業：清華大學長聘教授、博士生導師，美國普林斯頓大學訪問學者
- 性別：男
教育背景,工作履歷,所授課程,研究領域,研究概況,獲得榮譽,學術成果,
教育背景
2000年-2006年，北京航空航天大學，能源與動力工程學院
1996年-2000年，西北工業大學，能源與動力工程學院
工作履歷
2018.12-至今， 清華大學航天航空學院（雙聘），長聘教授/博導
2018.12-至今， 清華大學汽車工程系，長聘教授/博導
2016.12-2018.11，清華大學汽車工程系，長聘副教授/博導
2013.09-2016.11，清華大學汽車工程系，副研究員/博導
2010.12-2013.08，清華大學汽車工程系，副研究員/碩導
2008.04-2010.11，清華大學汽車工程系，助理研究員/碩導
2006.04-2008.03，清華大學汽車工程系，博士後
2011.07-2012.07， 普林斯頓大學，訪問學者
所授課程
《計算流體力學》
《發動機渦輪增壓技術》
研究領域
先進航空渦輪發動機（渦軸、渦槳、渦噴、渦扇）與葉輪機械技術
先進節能內燃機（汽油、柴油、氫能）與渦輪增壓技術
先進車用/航空發動機混合動力技術
新能源燃料電池渦輪增壓技術
新能源車用微型燃氣輪機增程器技術
研究概況
主持國家“兩機”重大專項、國家自然科學基金、科技部、教育部、總裝、國防科工局、中國航空發動機集團、中國航天科工集團、中國第一汽車集團、IHI、博馬科技等國家、國防、國際各類課題40餘項。
獲得榮譽
(1) 入選國家“萬人計畫”科技創新領軍人才（2019年）
(2) 入選創新人才推進計畫中青年科技創新領軍人才（2018年）
(3) 入選美國航空航天學會AIAA Associate Fellow（2018年，中國3人）
(4) 榮獲首屆中國內燃機工業傑出科技創新獎（2018年）
(5) 榮獲中國內燃機學會突出貢獻獎（2017年，全國2人）
(6) 榮獲中國青年科技獎（2016年）
(7) 榮獲清華大學“青年教師教學優秀獎”（2015年，清華10人）
(8) 榮獲清華大學“學術新人獎”（2015年，清華10人）
(9) 榮獲國防科技進步三等獎（2015年）
(10) 榮獲中國內燃機學會史紹熙人才獎（2014年，全國3人）
(11) 榮獲美國機械工程師協會最佳論文獎（2013年）
(12) 榮獲國家科技進步二等獎（2013年）
(13) 榮獲國防科技進步一等獎（2013年）
(14) 入選教育部“新世紀優秀人才”支持計畫（2013年）
(15) 榮獲茅以升北京青年科技獎（2013年，北京15人）
(16) 榮獲英國機械工程師協會最佳論文獎（2011年）
(17) 榮獲山東省科技進步二等獎（2011年）
(18) 榮獲國防技術發明三等獎（2011年）
(19) 榮獲教育部霍英東基金（2010年）
(20) 榮獲全國優秀博士學位論文（2008年）
學術成果
共發表（含錄用）論文120餘篇，其中SCI收錄70篇，EI收錄110餘篇。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等國際權威期刊發表論文40餘篇。授權發明專利美國4項、日本5項、中國18項。代表性論文列表如下（*為通訊作者）：
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)
