基本信息
阳诚武 男 硕导 中国科学院工程热物理研究所
电子邮件： yangchengwu@iet.cn
通信地址： 01082543131
邮政编码： 100190
电子邮件： yangchengwu@iet.cn
通信地址： 01082543131
邮政编码： 100190
研究领域
叶轮机械气动热力学
涡轴发动机总体
招生信息
招生专业
080701-工程热物理
080703-动力机械及工程
082502-航空宇航推进理论与工程
080703-动力机械及工程
082502-航空宇航推进理论与工程
招生方向
航空发动机气动热力学
涡轴发动机总体设计
涡轴发动机总体设计
教育背景
2012-09--2015-06 中国科学院大学工程热物理研究所 研究生，工学博士
2008-09--2010-06 东北大学 研究生，工学硕士
2004-09--2008-06 沈阳航空航天大学 本科，工学学士
2008-09--2010-06 东北大学 研究生，工学硕士
2004-09--2008-06 沈阳航空航天大学 本科，工学学士
学历
研究生
学位
工学博士
工作经历
工作简历
2019-05~现在, 中国科学院工程热物理研究所, 高级工程师
2015-07~2019-05,中国科学院工程热物理研究所, 助理研究员
2010-07~2012-08,中国航发湖南动力机械研究所, 设计员
2015-07~2019-05,中国科学院工程热物理研究所, 助理研究员
2010-07~2012-08,中国航发湖南动力机械研究所, 设计员
教授课程
流体动力学测试技术
出版信息
发表论文
[1] Mingyang Wang, Xingen Lu, Chengwu Yang, Ge Han, Shengfeng Zhao, Yanfeng Zhang. Loss reduction in the compressor corner region via blade cooling. INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES. 2024, 第 3 作者261: http://dx.doi.org/10.1016/j.ijmecsci.2023.108676.
[2] Cheng, Hongzhi, Zhou, Chuangxin, Lu, Xingen, Zhao, Shengfeng, Han, Ge, Yang, Chengwu. Robust aerodynamic optimization and design exploration of a wide-chord transonic fan under geometric and operational uncertainties. ENERGY[J]. 2023, 第 6 作者278: http://dx.doi.org/10.1016/j.energy.2023.128011.
[3] Mingyang Wang, Xingen Lu, Chengwu Yang, Shengfeng Zhao, Yanfeng Zhang. Control of separated flow transition over a highly loaded compressor blade via dynamic surface deformation. INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES. 2023, 第 3 作者241: http://dx.doi.org/10.1016/j.ijmecsci.2022.107980.
[4] Xu, Huafeng, Zhao, Shengfeng, Wang, Mingyang, Yang, Chengwu. Effects of Bionic Leading Edge on the Aerodynamic Performance of a Compressor Cascade at a Low Reynolds Number. JOURNAL OF THERMAL SCIENCE. 2023, 第 4 作者http://dx.doi.org/10.1007/s11630-023-1920-x.
[5] Han, Ge, Yang, Chengwu, Wu, Shixun, Zhao, Shengfeng, Lu, Xingen. The investigation of mechanisms on pipe diffuser leading edge vortex generation and development in centrifugal compressor. APPLIED THERMAL ENGINEERING[J]. 2023, 第 2 作者219: http://dx.doi.org/10.1016/j.applthermaleng.2022.119606.
[6] Mingyang Wang, Xingen Lu, Yang, Chengwu, Ge Han, Zhao Shengfeng, Yanfeng Zhang. Loss Reduction in the Compressor Corner Region via Blade Cooling. International Journal of Mechanical Sciences[J]. 2023, 第 3 作者241:
[7] Ge Han, Yang Chengwu, Shixun Wu, Shengfeng Zhao, Xingen Lu. The investigation of mechanisms on pipe diffuser leading edge vortex generation and development in centrifugal compressor. Applied Thermal Engineering[J]. 2022, 第 2 作者219(2023):
[8] Mingyang Wang, Xingen Lu, Yang Chengwu, Shengfeng Zhao, Yanfeng Zhang. Control of separated flow transition over a highly loaded compressor blade via dynamic surface deformation. International Journal of Mechanical Sciences[J]. 2022, 第 3 作者241(2023):
[9] Huang, Song, Lu, Xingen, Han, Ge, Zhao, Shengfeng, Zhou, Chuangxin, Yang, Chengwu. Research on aerodynamic optimization design method and flow mechanism of a high-subsonic compressor cascade. ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS[J]. 2022, 第 6 作者 通讯作者 16(1): 316-334, http://dx.doi.org/10.1080/19942060.2021.2020170.
[10] Wang, Mingyang, LI, Ziliang, Han, Ge, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Vortex dynamics and entropy generation in separated transitional flow over a compressor blade at various incidence angles. CHINESE JOURNAL OF AERONAUTICS[J]. 2022, 第 4 作者35(3): 42-52, http://dx.doi.org/10.1016/j.cja.2021.06.021.
[11] Jinxin Cheng, Shengfeng Zhao, Zhaohui Dong, Chengwu Yang. Design Optimization of a Multistage Axial Flow Compressor Based on Full-Blade Surface Parameterization and Phased Strategy. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING[J]. 2021, 第 4 作者2021: http://dx.doi.org/10.1155/2021/5583681.
[12] HUANG Song, YANG Chengwu, LI Ziliang, HAN Ge, ZHAO Shengfeng, LU Xingen. Effect of Non-Axisymmetric End Wall on a Highly Loaded Compressor Cascade in Multi-Conditions. JOURNAL OF THERMAL SCIENCE[J]. 2021, 第 2 作者 通讯作者 30(4): 1363-1375, http://dx.doi.org/10.1007/s11630-021-1448-x.
[13] Han, Ge, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Investigation of a High Pressure Ratio Centrifugal Compressor with Wedge Diffuser and Pipe Diffuser. INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES[J]. 2021, 第 2 作者38(1): 1-13, https://www.webofscience.com/wos/woscc/full-record/WOS:000621716800001.
[14] Wang, Mingyang, Lu, Xingen, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng. Numerical investigation of distributed roughness effects on separated flow transition over a highly loaded compressor blade. PHYSICS OF FLUIDS[J]. 2021, 第 3 作者33(11):
[15] Wang, Mingyang, Yang, Chengwu, Li, Ziliang, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number. CHINESE JOURNAL OF AERONAUTICS[J]. 2021, 第 2 作者34(3): 71-81, http://dx.doi.org/10.1016/j.cja.2020.08.020.
[16] Cheng Jinxin, Yang Chengwu, Zhao Shengfeng. A Phased Aerodynamic Optimization Method for Compressors Based on Multi-Degrees-of-Freedom Surface Parameterization. JOURNAL OF THERMAL SCIENCE[J]. 2021, 第 2 作者30(6): 2071-2086, http://dx.doi.org/10.1007/s11630-021-1479-3.
[17] Wang, Mingyang, Li, Ziliang, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Large eddy simulation of the separated flow transition on the suction surface of a high subsonic compressor airfoil. PHYSICS OF FLUIDS[J]. 2020, 第 3 作者32(3): https://www.webofscience.com/wos/woscc/full-record/WOS:000522041100001.
[18] Wang, Mingyang, Li, Ziliang, Yang, Chengwu, Han, Ge, Zhao, Shengfeng, Lu, Xingen. Numerical investigations of the separated transitional flow over compressor blades with different loading distributions. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 第 3 作者106: http://dx.doi.org/10.1016/j.ast.2020.106113.
[19] Huang, Song, Cheng, Jinxin, Yang, Chengwu, Zhou, Chuangxin, Zhao, Shengfeng, Lu, Xingen. Optimization Design of a 2.5 Stage Highly Loaded Axial Compressor with a Bezier Surface Modeling Method. APPLIED SCIENCES-BASEL[J]. 2020, 第 3 作者10(11): http://dx.doi.org/10.3390/app10113860.
[20] 黄松, 阳诚武, 韩戈, 赵胜丰, 卢新根. 静叶轮毂间隙对高负荷压气机性能的影响研究. 工程热物理学报[J]. 2020, 第 2 作者41(11): 2662-2669, http://lib.cqvip.com/Qikan/Article/Detail?id=7103289421.
[21] 黄松, 阳诚武, 韩戈, 赵胜丰, 王名扬, 卢新根. 采用鲸鱼算法的可控扩散叶型优化设计. 西安交通大学学报[J]. 2020, 第 2 作者54(3): 49-57, https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFDLAST2020&filename=XAJT202003007&v=MTczNTQ5Rlk0UjhlWDFMdXhZUzdEaDFUM3FUcldNMUZyQ1VSN3FlWitkcEZpbmxVTHZCUFN6QmVyRzRITkhNckk=.
[22] Li, Ziliang, Lu, Xingen, Han, Ge, Huang, Enliang, Yang, Chengwu, Zhu, Junqiang. Numerical and experimental investigation of flow mechanism and application of tandem-impeller for centrifugal compressor. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 第 5 作者100: http://dx.doi.org/10.1016/j.ast.2020.105819.
[23] Li, Ziliang, Zhao, Shengfeng, Lu, Xingen, Han, Ge, Yang, Chengwu, Zhu, Junqiang. Inducer/Exducer Matching Characteristics inside Tandem Impellers of a Highly Loaded Centrifugal Compressor. JOURNAL OF THERMAL SCIENCE[J]. 2020, 第 5 作者29(4): 928-944, http://lib.cqvip.com/Qikan/Article/Detail?id=7102368066.
[24] Huang, Song, Yang, Chengwu, Han, Ge, Zhao, Shengfeng, Lu, Xingen. Multipoint design optimization for a controlled diffusion airfoil compressor cascade. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE[J]. 2020, 第 2 作者 通讯作者 234(11): 2143-2159, https://www.webofscience.com/wos/woscc/full-record/WOS:000512856600001.
[25] Li, Ziliang, Lu, Xingen, Zhao, Shengfeng, Han, Ge, Yang, Chengwu, Zhang, Yanfeng. Numerical investigation of flow mechanisms of tandem impeller inside a centrifugal compressor. CHINESE JOURNAL OF AERONAUTICS[J]. 2019, 第 5 作者32(12): 2627-2640, http://lib.cqvip.com/Qikan/Article/Detail?id=7100901994.
[26] Yang Chengwu, Han Ge, Zhao Shengfeng, Lu Xingen, Zhang Yanfeng, Li Ziliang, ASME. DESIGN AND TEST OF A NOVEL HIGHLY-LOADED COMPRESSOR. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 2A. 2019, 第 1 作者http://apps.webofknowledge.com/CitedFullRecord.do?product=UA&colName=WOS&SID=5CCFccWmJJRAuMzNPjj&search_mode=CitedFullRecord&isickref=WOS:000501627800024.
[27] Li, Ziliang, Lu, Xingen, Zhang, Yanfeng, Han, Ge, Yang, Chengwu, Zhao, Shengfeng. Numerical investigation of a highly loaded centrifugal compressor stage with a tandem bladed impeller. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2018, 第 5 作者232(3): 240-253, https://www.webofscience.com/wos/woscc/full-record/WOS:000435491500003.
[28] Han, Ge, Yang, Chengwu, Li, Ziliang, Zhang, Yingjie, Zhao, Shengfeng, Lu, Xingen. High-pressure ratio centrifugal compressor with two different fishtail pipe diffuser configurations. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2018, 第 2 作者232(7): 785-798, https://www.webofscience.com/wos/woscc/full-record/WOS:000452792800002.
[29] Han, Ge, Lu, Xingen, Zhang, Yanfeng, Zhao, Shengfeng, Yang, Chengwu, Zhu, Junqiang. Investigation of two pipe diffuser configurations for a compact centrifugal compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2018, 第 5 作者232(4): 716-728, https://www.webofscience.com/wos/woscc/full-record/WOS:000429915700008.
[30] 韩建涛, 王晏根, 阳诚武, 李紫良, 朱俊强. 跨音速涡轮平面叶栅风洞收缩段设计方法研究. 燃气轮机技术[J]. 2017, 第 3 作者30(2): 17-22, http://lib.cqvip.com/Qikan/Article/Detail?id=672578477.
[31] 韩戈, 阳诚武, 李紫良, 赵胜丰, 卢新根. 离心压气机管式扩压器研究进展及评述. 航空学报[J]. 2017, 第 2 作者38(9): 46-57, https://d.wanfangdata.com.cn/periodical/hkxb201709004.
[32] 阳诚武. Design and Experimental Test of a 2.5-Stage Highly Loaded Axial Compressor. Proceedings of Shanghai 2017 Global Power and Propulsion Forum. 2017, 第 1 作者
[33] 王立志, 阳诚武, 张香华, 路纵横. 级负荷系数为0.42的小流量轴流压气机设计与试验验证. 航空发动机[J]. 2016, 第 2 作者42(3): 54-60, http://lib.cqvip.com/Qikan/Article/Detail?id=668890384.
[34] Chengwu Yang, Xingen Lu, Shengfeng Zhao, Yanfeng Zhang, Junqiang Zhu. Numerical Investigation of a Cantilevered Compressor Stator at Varying Clearance Sizes. ASME. 2015, 第 1 作者http://ir.etp.ac.cn/handle/311046/111275.
[35] 阳诚武, 赵胜丰, 韩戈, 卢新根, 朱俊强. 跨声速压气机多圆柱孔式处理机匣设计与扩稳机理研究. 推进技术[J]. 2015, 第 1 作者36(3): 385-391, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=5364279&detailType=1.
[36] Zhao, Shengfeng, Lu, Xingen, Zhu, Junqiang, Ge, Han, Yang Chengwu. Effects of low Reynolds number on flow stability of a transonic compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2015, 第 5 作者229(4): 601-611, http://ir.etp.ac.cn/handle/311046/98931.
[37] 杨家礼, 涂孟罴, 张亿力, 张立章, 阳诚武. 一种涡轮叶尖间隙控制技术. 航空动力学报[J]. 2014, 第 5 作者29(9): 2195-2201, https://d.wanfangdata.com.cn/periodical/hkdlxb201409025.
[38] 韩戈, 卢新根, 赵胜丰, 阳诚武, 朱俊强. 喉部长度和扩张角对离心压气机管式扩压器影响研究. 推进技术[J]. 2014, 第 4 作者35(12): 1607-1614, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=5306944&detailType=1.
[39] Yang Chengwu, Zhao Shengfeng, Lu Xingen, Han Ge, Zhu Junqiang. Investigation on Multiple Cylindrical Holes Casing Treatment for Transonic Axial Compressor Stability Enhancement. JOURNAL OF THERMAL SCIENCE[J]. 2014, 第 1 作者 通讯作者 23(4): 346-353, http://www.irgrid.ac.cn/handle/1471x/994088.
[40] 韩戈, 卢新根, 赵胜丰, 阳诚武, 朱俊强. 喉部长度和扩张角对离心压气机管式扩压器影响研究. 推进技术[J]. 2014, 第 4 作者1607-1614, http://lib.cqvip.com/Qikan/Article/Detail?id=84747483504849524950484852.
[41] Han, Ge, Lu, Xingen, Zhao, Shengfeng, Yang, Chengwu, Zhu, Junqiang. Parametric Studies of Pipe Diffuser on Performance of a Highly Loaded Centrifugal Compressor. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME[J]. 2014, 第 4 作者136(12): http://ir.etp.ac.cn/handle/311046/106010.
[2] Cheng, Hongzhi, Zhou, Chuangxin, Lu, Xingen, Zhao, Shengfeng, Han, Ge, Yang, Chengwu. Robust aerodynamic optimization and design exploration of a wide-chord transonic fan under geometric and operational uncertainties. ENERGY[J]. 2023, 第 6 作者278: http://dx.doi.org/10.1016/j.energy.2023.128011.
[3] Mingyang Wang, Xingen Lu, Chengwu Yang, Shengfeng Zhao, Yanfeng Zhang. Control of separated flow transition over a highly loaded compressor blade via dynamic surface deformation. INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES. 2023, 第 3 作者241: http://dx.doi.org/10.1016/j.ijmecsci.2022.107980.
[4] Xu, Huafeng, Zhao, Shengfeng, Wang, Mingyang, Yang, Chengwu. Effects of Bionic Leading Edge on the Aerodynamic Performance of a Compressor Cascade at a Low Reynolds Number. JOURNAL OF THERMAL SCIENCE. 2023, 第 4 作者http://dx.doi.org/10.1007/s11630-023-1920-x.
[5] Han, Ge, Yang, Chengwu, Wu, Shixun, Zhao, Shengfeng, Lu, Xingen. The investigation of mechanisms on pipe diffuser leading edge vortex generation and development in centrifugal compressor. APPLIED THERMAL ENGINEERING[J]. 2023, 第 2 作者219: http://dx.doi.org/10.1016/j.applthermaleng.2022.119606.
[6] Mingyang Wang, Xingen Lu, Yang, Chengwu, Ge Han, Zhao Shengfeng, Yanfeng Zhang. Loss Reduction in the Compressor Corner Region via Blade Cooling. International Journal of Mechanical Sciences[J]. 2023, 第 3 作者241:
[7] Ge Han, Yang Chengwu, Shixun Wu, Shengfeng Zhao, Xingen Lu. The investigation of mechanisms on pipe diffuser leading edge vortex generation and development in centrifugal compressor. Applied Thermal Engineering[J]. 2022, 第 2 作者219(2023):
[8] Mingyang Wang, Xingen Lu, Yang Chengwu, Shengfeng Zhao, Yanfeng Zhang. Control of separated flow transition over a highly loaded compressor blade via dynamic surface deformation. International Journal of Mechanical Sciences[J]. 2022, 第 3 作者241(2023):
[9] Huang, Song, Lu, Xingen, Han, Ge, Zhao, Shengfeng, Zhou, Chuangxin, Yang, Chengwu. Research on aerodynamic optimization design method and flow mechanism of a high-subsonic compressor cascade. ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS[J]. 2022, 第 6 作者 通讯作者 16(1): 316-334, http://dx.doi.org/10.1080/19942060.2021.2020170.
[10] Wang, Mingyang, LI, Ziliang, Han, Ge, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Vortex dynamics and entropy generation in separated transitional flow over a compressor blade at various incidence angles. CHINESE JOURNAL OF AERONAUTICS[J]. 2022, 第 4 作者35(3): 42-52, http://dx.doi.org/10.1016/j.cja.2021.06.021.
[11] Jinxin Cheng, Shengfeng Zhao, Zhaohui Dong, Chengwu Yang. Design Optimization of a Multistage Axial Flow Compressor Based on Full-Blade Surface Parameterization and Phased Strategy. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING[J]. 2021, 第 4 作者2021: http://dx.doi.org/10.1155/2021/5583681.
[12] HUANG Song, YANG Chengwu, LI Ziliang, HAN Ge, ZHAO Shengfeng, LU Xingen. Effect of Non-Axisymmetric End Wall on a Highly Loaded Compressor Cascade in Multi-Conditions. JOURNAL OF THERMAL SCIENCE[J]. 2021, 第 2 作者 通讯作者 30(4): 1363-1375, http://dx.doi.org/10.1007/s11630-021-1448-x.
[13] Han, Ge, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Investigation of a High Pressure Ratio Centrifugal Compressor with Wedge Diffuser and Pipe Diffuser. INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES[J]. 2021, 第 2 作者38(1): 1-13, https://www.webofscience.com/wos/woscc/full-record/WOS:000621716800001.
[14] Wang, Mingyang, Lu, Xingen, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng. Numerical investigation of distributed roughness effects on separated flow transition over a highly loaded compressor blade. PHYSICS OF FLUIDS[J]. 2021, 第 3 作者33(11):
[15] Wang, Mingyang, Yang, Chengwu, Li, Ziliang, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number. CHINESE JOURNAL OF AERONAUTICS[J]. 2021, 第 2 作者34(3): 71-81, http://dx.doi.org/10.1016/j.cja.2020.08.020.
[16] Cheng Jinxin, Yang Chengwu, Zhao Shengfeng. A Phased Aerodynamic Optimization Method for Compressors Based on Multi-Degrees-of-Freedom Surface Parameterization. JOURNAL OF THERMAL SCIENCE[J]. 2021, 第 2 作者30(6): 2071-2086, http://dx.doi.org/10.1007/s11630-021-1479-3.
[17] Wang, Mingyang, Li, Ziliang, Yang, Chengwu, Zhao, Shengfeng, Zhang, Yanfeng, Lu, Xingen. Large eddy simulation of the separated flow transition on the suction surface of a high subsonic compressor airfoil. PHYSICS OF FLUIDS[J]. 2020, 第 3 作者32(3): https://www.webofscience.com/wos/woscc/full-record/WOS:000522041100001.
[18] Wang, Mingyang, Li, Ziliang, Yang, Chengwu, Han, Ge, Zhao, Shengfeng, Lu, Xingen. Numerical investigations of the separated transitional flow over compressor blades with different loading distributions. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 第 3 作者106: http://dx.doi.org/10.1016/j.ast.2020.106113.
[19] Huang, Song, Cheng, Jinxin, Yang, Chengwu, Zhou, Chuangxin, Zhao, Shengfeng, Lu, Xingen. Optimization Design of a 2.5 Stage Highly Loaded Axial Compressor with a Bezier Surface Modeling Method. APPLIED SCIENCES-BASEL[J]. 2020, 第 3 作者10(11): http://dx.doi.org/10.3390/app10113860.
[20] 黄松, 阳诚武, 韩戈, 赵胜丰, 卢新根. 静叶轮毂间隙对高负荷压气机性能的影响研究. 工程热物理学报[J]. 2020, 第 2 作者41(11): 2662-2669, http://lib.cqvip.com/Qikan/Article/Detail?id=7103289421.
[21] 黄松, 阳诚武, 韩戈, 赵胜丰, 王名扬, 卢新根. 采用鲸鱼算法的可控扩散叶型优化设计. 西安交通大学学报[J]. 2020, 第 2 作者54(3): 49-57, https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFDLAST2020&filename=XAJT202003007&v=MTczNTQ5Rlk0UjhlWDFMdXhZUzdEaDFUM3FUcldNMUZyQ1VSN3FlWitkcEZpbmxVTHZCUFN6QmVyRzRITkhNckk=.
[22] Li, Ziliang, Lu, Xingen, Han, Ge, Huang, Enliang, Yang, Chengwu, Zhu, Junqiang. Numerical and experimental investigation of flow mechanism and application of tandem-impeller for centrifugal compressor. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 第 5 作者100: http://dx.doi.org/10.1016/j.ast.2020.105819.
[23] Li, Ziliang, Zhao, Shengfeng, Lu, Xingen, Han, Ge, Yang, Chengwu, Zhu, Junqiang. Inducer/Exducer Matching Characteristics inside Tandem Impellers of a Highly Loaded Centrifugal Compressor. JOURNAL OF THERMAL SCIENCE[J]. 2020, 第 5 作者29(4): 928-944, http://lib.cqvip.com/Qikan/Article/Detail?id=7102368066.
[24] Huang, Song, Yang, Chengwu, Han, Ge, Zhao, Shengfeng, Lu, Xingen. Multipoint design optimization for a controlled diffusion airfoil compressor cascade. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE[J]. 2020, 第 2 作者 通讯作者 234(11): 2143-2159, https://www.webofscience.com/wos/woscc/full-record/WOS:000512856600001.
[25] Li, Ziliang, Lu, Xingen, Zhao, Shengfeng, Han, Ge, Yang, Chengwu, Zhang, Yanfeng. Numerical investigation of flow mechanisms of tandem impeller inside a centrifugal compressor. CHINESE JOURNAL OF AERONAUTICS[J]. 2019, 第 5 作者32(12): 2627-2640, http://lib.cqvip.com/Qikan/Article/Detail?id=7100901994.
[26] Yang Chengwu, Han Ge, Zhao Shengfeng, Lu Xingen, Zhang Yanfeng, Li Ziliang, ASME. DESIGN AND TEST OF A NOVEL HIGHLY-LOADED COMPRESSOR. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 2A. 2019, 第 1 作者http://apps.webofknowledge.com/CitedFullRecord.do?product=UA&colName=WOS&SID=5CCFccWmJJRAuMzNPjj&search_mode=CitedFullRecord&isickref=WOS:000501627800024.
[27] Li, Ziliang, Lu, Xingen, Zhang, Yanfeng, Han, Ge, Yang, Chengwu, Zhao, Shengfeng. Numerical investigation of a highly loaded centrifugal compressor stage with a tandem bladed impeller. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2018, 第 5 作者232(3): 240-253, https://www.webofscience.com/wos/woscc/full-record/WOS:000435491500003.
[28] Han, Ge, Yang, Chengwu, Li, Ziliang, Zhang, Yingjie, Zhao, Shengfeng, Lu, Xingen. High-pressure ratio centrifugal compressor with two different fishtail pipe diffuser configurations. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2018, 第 2 作者232(7): 785-798, https://www.webofscience.com/wos/woscc/full-record/WOS:000452792800002.
[29] Han, Ge, Lu, Xingen, Zhang, Yanfeng, Zhao, Shengfeng, Yang, Chengwu, Zhu, Junqiang. Investigation of two pipe diffuser configurations for a compact centrifugal compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2018, 第 5 作者232(4): 716-728, https://www.webofscience.com/wos/woscc/full-record/WOS:000429915700008.
[30] 韩建涛, 王晏根, 阳诚武, 李紫良, 朱俊强. 跨音速涡轮平面叶栅风洞收缩段设计方法研究. 燃气轮机技术[J]. 2017, 第 3 作者30(2): 17-22, http://lib.cqvip.com/Qikan/Article/Detail?id=672578477.
[31] 韩戈, 阳诚武, 李紫良, 赵胜丰, 卢新根. 离心压气机管式扩压器研究进展及评述. 航空学报[J]. 2017, 第 2 作者38(9): 46-57, https://d.wanfangdata.com.cn/periodical/hkxb201709004.
[32] 阳诚武. Design and Experimental Test of a 2.5-Stage Highly Loaded Axial Compressor. Proceedings of Shanghai 2017 Global Power and Propulsion Forum. 2017, 第 1 作者
[33] 王立志, 阳诚武, 张香华, 路纵横. 级负荷系数为0.42的小流量轴流压气机设计与试验验证. 航空发动机[J]. 2016, 第 2 作者42(3): 54-60, http://lib.cqvip.com/Qikan/Article/Detail?id=668890384.
[34] Chengwu Yang, Xingen Lu, Shengfeng Zhao, Yanfeng Zhang, Junqiang Zhu. Numerical Investigation of a Cantilevered Compressor Stator at Varying Clearance Sizes. ASME. 2015, 第 1 作者http://ir.etp.ac.cn/handle/311046/111275.
[35] 阳诚武, 赵胜丰, 韩戈, 卢新根, 朱俊强. 跨声速压气机多圆柱孔式处理机匣设计与扩稳机理研究. 推进技术[J]. 2015, 第 1 作者36(3): 385-391, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=5364279&detailType=1.
[36] Zhao, Shengfeng, Lu, Xingen, Zhu, Junqiang, Ge, Han, Yang Chengwu. Effects of low Reynolds number on flow stability of a transonic compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2015, 第 5 作者229(4): 601-611, http://ir.etp.ac.cn/handle/311046/98931.
[37] 杨家礼, 涂孟罴, 张亿力, 张立章, 阳诚武. 一种涡轮叶尖间隙控制技术. 航空动力学报[J]. 2014, 第 5 作者29(9): 2195-2201, https://d.wanfangdata.com.cn/periodical/hkdlxb201409025.
[38] 韩戈, 卢新根, 赵胜丰, 阳诚武, 朱俊强. 喉部长度和扩张角对离心压气机管式扩压器影响研究. 推进技术[J]. 2014, 第 4 作者35(12): 1607-1614, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=5306944&detailType=1.
[39] Yang Chengwu, Zhao Shengfeng, Lu Xingen, Han Ge, Zhu Junqiang. Investigation on Multiple Cylindrical Holes Casing Treatment for Transonic Axial Compressor Stability Enhancement. JOURNAL OF THERMAL SCIENCE[J]. 2014, 第 1 作者 通讯作者 23(4): 346-353, http://www.irgrid.ac.cn/handle/1471x/994088.
[40] 韩戈, 卢新根, 赵胜丰, 阳诚武, 朱俊强. 喉部长度和扩张角对离心压气机管式扩压器影响研究. 推进技术[J]. 2014, 第 4 作者1607-1614, http://lib.cqvip.com/Qikan/Article/Detail?id=84747483504849524950484852.
[41] Han, Ge, Lu, Xingen, Zhao, Shengfeng, Yang, Chengwu, Zhu, Junqiang. Parametric Studies of Pipe Diffuser on Performance of a Highly Loaded Centrifugal Compressor. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME[J]. 2014, 第 4 作者136(12): http://ir.etp.ac.cn/handle/311046/106010.
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