郑新前，中国青年科技奖获得者，清华大学特别研究员（长聘）、博士生导师，普林斯顿大学访问学者，ASME Journal of Engineering for Gas Turbines and Power副主编，Aerospace Science and Technology副主编。面向国家重大需求和国际学术前沿，长期从事航空涡轮发动机和涡轮增压内燃机研究，主持国家、国防、国际等课题30余项；发表学术论文110余篇，SCI论文60余篇，授权发明专利美国4项、日本5项、中国16项。先后获得中国青年科技奖、国家科技进步二等奖、美国机械工程师协会最佳论文奖、英国机械工程师协会最佳论文奖、中国内燃机学会突出贡献奖、全国优秀博士学位论文、清华大学学术新人奖、清华大学青年教师教学优秀奖、国防科技进步一等奖、山东省科技进步二等奖、国防科技进步三等奖、国防技术发明三等奖、教育部霍英东基金、教育部新世纪优秀人才支持计划、茅以升北京青年科技奖、中国内燃机学会史绍熙人才奖等16项奖励。
教育背景
2016.07-2016.07，中国延安干部学院，中组部青年科技领军人才研修班；
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
2016.12-至今，清华大学汽车工程系，特别研究员（长聘）/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，访问学者。
所授课程
《内燃机增压与增压技术》；
《计算流体力学》。
研究领域
航空涡轮发动机（涡轴、涡桨、涡喷、涡轮风扇发动机）流动与叶轮机械技术；
内燃机（汽油、柴油、氢能）流动与涡轮增压技术；
车用/航空发动机混合动力技术；
燃料电池涡轮增压技术；
车用微型燃气轮机增程器技术。
研究概况
主持“两机”重大专项项目，此外还主持国家自然科学基金、科技部、教育部、总装、国家国防科技工业局、国际合作、中国航空发动机集团有限公司、中国航天科工集团有限公司、中国一汽等课题30余项。
获得荣誉
(1)中国内燃机学会突出贡献奖（2017年，全国2人）
(2)中国青年科技奖（2016年）
(3)清华大学“青年教师教学优秀奖”（2015年，共10人）
(4)清华大学“学术新人奖”（2015年，共10人）
(5)国防科技进步三等奖（2015年）
(6)内燃机学会史绍熙人才奖（2014年）
(7)美国机械工程师协会最佳论文奖（2013年）
(8)国家科技进步二等奖（2013年）
(9)国防科技进步一等奖（2013年）
(10)教育部“新世纪优秀人才”支持计划（2013年）
(11)茅以升北京青年科技奖（2013年）
(12)英国机械工程师协会最佳论文奖（2011年）
(13)山东省科技进步二等奖（2011年）
(14)国防技术发明三等奖（2011年）
(15)教育部霍英东基金（2010年）
(16)全国优秀博士学位论文（2008年）
学术成果
共发表（含录用）论文110余篇，其中SCI收录60篇，EI收录100余篇。在ASME Journal of Turbomachinery、AIAA Journal of Propulsion and 功率、Progress in Aerospace Sciences、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30余篇。授权发明专利美国4项、日本5项、中国16项。代表性论文列表如下（*为通讯作者）：
• ASME Journal of Turbomachinery
ZHENG Xinqian*, SUN Zhenzhong, KAWAKUBO Tomoki, TAMAKI Hideaki, “Stability Improvement of a Turbocharger Centrifugal Compressor by Non-Axisymmetric Vaned Diffuser,” Journal of 蝾螺属machinery-Transactions of the ASME, 2018, 140 (4): 041007-1~13. (SCI: ; EI:)
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)
ZHENG Xinqian*, Liu Anxiong, “Phenomenon and Mechanism of Two-Regime-Surge in a Centrifugal Compressor,” Journal of 蝾螺属machinery-Transactions of the ASME, 2015, 137 (8): 081007-1~7. (SCI: CL3FI; EI: 20152901032948)
ZHENG 辛姓qian*, ZHANG Yangjun, YANG Mingyang, BAMBA Takahiro, TAMAKI Hideaki, “Stability Improvement of High-压强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)
YANG Mingyang,ZHENG Xinqian*, ZHANG Yangjun, BAMBA 田崎敬浩, TAMAKI Hideaki, HUENTELER Joern, LI Zhigang, “Stability Improvement of High-压强Ratio 蝾螺属charger 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)
TAMAKI Hideaki*,ZHENG Xinqian, ZHANG Yangjun, “Experimental Investigation of High 压强 Ratio Centrifugal Compressor with Axisymmetric and Nonaxisymmetric Recirculation Device,” Journal of 蝾螺属machinery-Transactions of the ASME, 2013, 135 (3): 031023-1~12. (SCI: 239KD; EI: 20133316600816)
ZHENG 辛姓qian*, 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)
ZHENG Xinqian*, ZHOU 盛姓, LU Yajun, HOU Anping, LI Qiushi, “Flow Control of Annular Compressor Cascade by Synthetic Jets,” Journal of 蝾螺属machinery-Transactions of the ASME, 2008, 130 (2): 021018-1~7. (SCI: 279UP; EI: 20083111418141)
ZHENG 辛姓qian*, 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)
• AIAA Journal of Propulsion and 功率
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)
HUANG Qiangqiang,ZHENG 辛姓qian*, “Potential of Variable Geometry Method on Compressor Range Extension for 蝾螺属charged Engines,” AIAA Journal of Propulsion and 功率, 2017, 33 (5): 1197-1206. (SCI: FE6JA, EI:20173504098403)
HE Xiao,ZHENG Xinqian*, “The Mechanisms of Lean on the 表演 of Transonic Centrifugal Compressor Impellers,” AIAA Journal of Propulsion and Power, 2016, 32 (5): 1220-1229. (SCI: DW2MH; EI: 20163502763102)
YANG Mingyang*, MARTINEZ-BOTAS P·里卡多, ZHANG Yangjun,ZHENG 辛姓qian, “Effect of Self-Recirculation-Casing Treatment on High 压强 Ratio Centrifugal Compressor,” AIAA Journal of Propulsion and 功率, 2016, 32 (3): 602-610. (SCI: DM9GH; EI: 20162102420993)
ZHENG Xinqian*, LIU Anxiong, “Experimental Investigation of Surge and Stall in a High-Speed Centrifugal Compressor,” AIAA Journal of Propulsion and 功率, 2015, 31 (3): 815-825. (SCI: CQ8ES; EI: 20152000847455
• Progress in Aerospace Sciences
ZHENG Xinqian*, LI Zhihui, “Blade-end Treatment to Improve the 表演 of Axial Compressors: An Overview,” Progress in Aerospace Sciences, 2017, 88: 1–14. (SCI: EI8PY; EI: 20165003110729)
LI Zhihui,ZHENG Xinqian*, “Review of 设计 Optimization Methods for Turbomachinery 空气动力学,” Progress in Aerospace Sciences, 2017, 93: 1-23. (SCI: FI8QC ; EI: 20172903947521)
• 能量
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
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)
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
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)
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)
MOSTAFA Moosania,ZHENG Xinqian*, “Effect of Internal Heat leakage on the 表演 of a High 压强 Ratio Centrifugal Compressor,” Applied Thermal Engineering, 2017, 111: 317-324. (SCI: EH6PU;EI:20163902856012)
• IMechE Part A: Journal of 功率 and 能量
ZHENG Xinqian*, JIN Lei, TAMAKI Hideaki, “Influence of Volute-Induced Distortion on the 表演 of a High-压强ratio Centrifugal Compressor with a Vaneless Diffuser for Turbocharger Applications,” IMechE Part A: Journal of 功率 and 能量, 2014, 228 (4): 440-450. (SCI: AG8GH; EI: 20141917699337)
YANG Dong,ZHENG Xinqian, LI Qiushi*, “An 11-Stage Axial Compressor 表演 Simulation Considering the Change of Tip Clearance in Different Operating Conditions,” IMechE Part A: Journal of 功率 and 能量, 2014, 228 (6): 614-625. (SCI: AM8YT; EI: 20143118009029)
ZHENG Xinqian*, HUENTELE Joern, YANG Mingyang, ZHANG Yangjun, BAMBA Takahiro, “Influence of the Volute on the Flow in a Centrifugal Compressor of a High-压强 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
WANG Aolin,ZHENG Xinqian*, “设计 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:)
SUN Zhenzhong,ZHENG Xinqian*, LINGHU Zelin, KAWAKUBO Tomoki, TAMAKI Hideaki, WANG Baotong, “Influence of Volute 设计 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:)
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)
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)
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)
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)
ZHENG Xinqian*, LAN Chuanjie, “Improvement in the 表演 of a High-压强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)
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
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:)
ZHENGXinqian*, LIN Yun, SUN Zhenzhong, “Effects of Volute’s Asymmetry on the 表演 of a Turbocharger Centrifugal Compressor,” IMechE Part G: Journal of Aerospace Engineering, 2018, Online, DOI: 10.1177/0954410016670418. (SCI; EI)
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)
ZHENG Xinqian*, DING 壮语, 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)
MOSTAFA Moosania,ZHENG Xinqian*, “表演 Improvement of a High 压强 Ratio Centrifugal Compressor by Integrated Cooling,” IMechE Part G: Journal of Aerospace Engineering, 2016, 230 (12): 2233–2240. (SCI: DV5LV; EI: 20163702804198)
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)
LU Hanan,ZHENG Xinqian, LI Qiushi*, “A Combinatorial Optimization 设计 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
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: )
ZHENG Xinqian*, LAN ChuanJie, “Effects of Blade Bowing on the 表演 of a High 压强Ratio Turbocharger Centrifugal Compressor with Self-recirculation Casing Treatment,” Sci China Ser E-Tech Sci, 2013, 56 (10): 2531-2539. (SCI: 227PL; EI: 20134216867928)
ZHENG Xinqian*, LIN Yun, GAN Binlin, ZHUGE Weilin, ZHANG Yangjun, “Effects of Reynolds Number on the 表演 of a High 压强Ratio Turbocharger Compressor,” Sci China Ser E-Tech Sci, 2013, 56 (6): 1361-1369. (SCI: 168WR; EI: 20132816483688)
ZHENG Xinqian*, JIN Lei, TAMAKI Hideaki, “Influence of Volute Distortion on the 表演 of Turbocharger Centrifugal Compressor with Vane Diffuser”, Sci China Ser E-Tech Sci, 2013, 56 (11): 2778-27869. (SCI: 245JL; EI: 20134817033077)
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 表演 of a High 压强 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 压强 Ratio Turbocharger for Vehicle Internal Combustion Engines,” Sci China Ser E-Tech Sci, 2010, 53 (7): 1817-1823. (SCI: 621SZ; EI: 20103313151379)