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。
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。
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。
《内燃机增压与增压技术》；
《计算流体力学》。
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。
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。
(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）
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)