基本信息
项效镕 男 硕导 中国科学院工程热物理研究所
电子邮件： xiangxiaorong@iet.cn
通信地址： 北京市海淀区北四环西路11号
邮政编码：
电子邮件： xiangxiaorong@iet.cn
通信地址： 北京市海淀区北四环西路11号
邮政编码：
研究领域
航空发动机压气机非定常流动机制与实验测试技术研究
招生信息
招生专业
080701-工程热物理
招生方向
航空发动机试验与测试
教育背景
2005-09--2010-12 西北工业大学动力与能源学院 研究生，工学博士
2001-09--2005-07 西北工业大学动力与能源学院 本科，工学学士
2001-09--2005-07 西北工业大学动力与能源学院 本科，工学学士
学历
研究生
学位
博士
工作经历
工作简历
2021-06~现在, 中国科学院工程热物理研究所, 正高级工程师
2016-01~2021-05,中国科学院工程热物理研究所, 高级工程师
2011-02~2015-12,中国科学院工程热物理研究所, 助理研究员
2016-01~2021-05,中国科学院工程热物理研究所, 高级工程师
2011-02~2015-12,中国科学院工程热物理研究所, 助理研究员
专利与奖励
出版信息
发表论文
[1] Zhang, Yuankun, Zhao, Qingjun, Hu, Bin, Shi, Qiang, Zhao, Wei, Xiang, Xiaorong. Effects of Local Mixing Ratios and Mass Flow Rates on Combustion Performance of the Fuel-Rich LOX (Liquid Oxygen)/kerosene Gas Generator in the ATR (Air Turbo Rocket) Engine. AEROSPACE[J]. 2023, 10(6): http://dx.doi.org/10.3390/aerospace10060545.
[2] Ren, Sanqun, Xiang, Xiaorong, Zhao, Qingjun, Wang, Weimin, Zhao, Wei, Zhan, Chuanlin. Multi-probe linear fitting and time of arrival linear correction method to analyze blade vibration based on blade tip timing without once-per-revolution. CHINESE JOURNAL OF AERONAUTICS[J]. 2023, 36(1): 290-310, http://dx.doi.org/10.1016/j.cja.2022.06.006.
[3] Zhou, Xiaoxiao, Zhao, Qingjun, Xu, Qiangren, Wang, Yimeng, Zhao, Wei, Xiang, Xiaorong. Hub aspiration strategies and flow loss analysis of a shock-in type supersonic compressor rotor with negative inlet pre-whirl. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY. 2022, [4] Zhao, Qingjun, Cui, Weiwei, Xiang, Xiaorong, Xu, Qiangren, Xu, Jianzhong. Numerical investigation of blade tip winglet on flow structure in a high loading transonic rotor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2022, 236(1): 96-108, http://dx.doi.org/10.1177/09544100211008093.
[5] Ren, Sanqun, Xiang, Xiaorong, Zhao, Qingjun, Wang, Weimin, Zhao, Wei, Hao, Long. Research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces. JOURNAL OF LOW FREQUENCY NOISE VIBRATION AND ACTIVE CONTROL[J]. 2021, 40(4): 2077-2093, http://apps.webofknowledge.com/CitedFullRecord.do?product=UA&colName=WOS&SID=5CCFccWmJJRAuMzNPjj&search_mode=CitedFullRecord&isickref=WOS:000680723600001.
[6] Zhao, Qingjun, Cui, Weiwei, Xiang, Xiaorong, Xu, Qiangren, Xu, Jianzhong. Numerical investigation of blade tip winglet on flow structure in a high loading transonic rotor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2021, [7] Liu, Zhiyuan, Zhao, Qingjun, Xiang, Xiaorong, Zhao, Wei, Zhou, Xiaoyong. A hybrid viscous body force model for low-speed centrifugal compressors. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2021, 235(3): 335-350, https://www.webofscience.com/wos/woscc/full-record/WOS:000554549600001.
[8] Zhao, Qingjun, Cui, Weiwei, Zhao, Wei, Xiang, Xiaorong, Xu, Jianzhong. Investigation on the effects of winglet geometry in a high loading compressor rotor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2021, 235(8): 1819-1831, http://dx.doi.org/10.1177/09576509211017004.
[9] Sui, Xiuming, Zhao, Wei, Xiang, Xiaorong, Pi, Te, Zhao, Qingjun. Investigation of the flowfield on a vaneless counter-rotating turbine with seal cavity flow ejection. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2021, 235(8): 1864-1876, http://dx.doi.org/10.1177/09576509211018307.
[10] 徐强仁, 刘智远, 项效镕, 周小勇, 赵庆军. 对转压气机外伸激波对叶顶泄漏流影响. 航空动力学报[J]. 2019, 2027-2037, http://lib.cqvip.com/Qikan/Article/Detail?id=72756873504849574857485048.
[11] Kai Zhang, Yingqun Ma, Xiaorong Xiang, Wei Zhao, Qingjun Zhao. Research on Transient Vibration Response of Rotor System Using Supporting Stiffness Active Control. AIAA Propulsion and Energy Forum 2018 Joint Propulsion Conferencenull. 2018, [12] 徐强仁, 马英群, 叶树波, 项效镕, 赵庆军. 高负荷对转压气机尾迹涡级间迁移影响因素研究. 推进技术[J]. 2018, 39(12): 2737-2745, http://lib.cqvip.com/Qikan/Article/Detail?id=6100107587.
[13] Wang, Yunfei, Sui, Xiuming, Zhang, Kai, Xiang, Xiaorong, Zhao, Qingjun. Effects of incidence angle on a low-pressure turbine blade boundary layer evolution through large eddy simulation. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2018, 232(6): 722-734, https://www.webofscience.com/wos/woscc/full-record/WOS:000443311900010.
[14] Zhou, Xiaoyong, Zhao, Qingjun, Xiang, Xiaorong, Cui, Weiwei. Investigation of groove casing treatment in a transonic compressor at different speeds with control volume method. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2016, 230(13): 2392-2408, http://www.corc.org.cn/handle/1471x/2374961.
[15] 黄晨, 项效镕, 张彬彬, 赵巍, 赵庆军. 膨胀式空气涡轮火箭最大状态调节规律与性能分析. 工程热物理学报[J]. 2016, 37(10): 2070-2075, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=5825258&detailType=1.
[16] Cui, Weiwei, Xiang, Xiaorong, Zhao, Qingjun, Xu, Jianzhong. The effect of sweep on flowfields of a highly loaded transonic rotor. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2016, 58: 71-81, https://www.webofscience.com/wos/woscc/full-record/WOS:000388543700007.
[17] Zhang, Binbin, Zhao, Qingjun, Xiang, Xiaorong, Xu, Jianzhong. An improved micro-vortex generator in supersonic flows. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2015, 47: 210-215, http://ir.etp.ac.cn/handle/311046/112318.
[18] 黄晨, 项效镕, 张彬彬, 赵巍, 赵庆军. 基于预冷器特性的膨胀式空气涡轮火箭发动机性能分析. 2015年中国工程热物理学会气动学学术年会null. 2015, http://ir.etp.ac.cn/handle/311046/110974.
[19] Zhao, Qingjun, Zhou, Xiaoyong, Xiang, Xiaorong. Multi-objective optimization of groove casing treatment in a transonic compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2014, 228(6): 626-637, https://www.webofscience.com/wos/woscc/full-record/WOS:000340166200003.
[20] 崔伟伟, 项效镕, 杜建一, 徐建中. 掠效应对高负荷跨音转子性能的影响. 工程热物理学报[J]. 2012, 33(5): 753-756, http://lib.cqvip.com/Qikan/Article/Detail?id=41729095.
[21] 周小勇, 项效镕, 赵庆军. 基于人工神经网络的跨音压气机周向槽机匣处理优化设计. 中国工程热物理学会null. 2012, http://ir.etp.ac.cn/handle/311046/58082.
[22] Bo Liu, Lei Wang, Qingwei Wang, Xiaorong Xiang. Investigation of the Unsteady Flow in an Counter-Rotating Compressor Using the Nonlinear Harmonic Method. ISABEnull. 2011, http://ir.etp.ac.cn/handle/311046/81861.
[23] Liu Bo, Hou Weimin, Nan Xiangyi, Xiang Xiaorong. Numerical and experimental investigation of the dual stage counter rotating compressor by boundary layer suction. ISABEnull. 2009, http://ir.etp.ac.cn/handle/311046/81477.
[2] Ren, Sanqun, Xiang, Xiaorong, Zhao, Qingjun, Wang, Weimin, Zhao, Wei, Zhan, Chuanlin. Multi-probe linear fitting and time of arrival linear correction method to analyze blade vibration based on blade tip timing without once-per-revolution. CHINESE JOURNAL OF AERONAUTICS[J]. 2023, 36(1): 290-310, http://dx.doi.org/10.1016/j.cja.2022.06.006.
[3] Zhou, Xiaoxiao, Zhao, Qingjun, Xu, Qiangren, Wang, Yimeng, Zhao, Wei, Xiang, Xiaorong. Hub aspiration strategies and flow loss analysis of a shock-in type supersonic compressor rotor with negative inlet pre-whirl. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY. 2022, [4] Zhao, Qingjun, Cui, Weiwei, Xiang, Xiaorong, Xu, Qiangren, Xu, Jianzhong. Numerical investigation of blade tip winglet on flow structure in a high loading transonic rotor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2022, 236(1): 96-108, http://dx.doi.org/10.1177/09544100211008093.
[5] Ren, Sanqun, Xiang, Xiaorong, Zhao, Qingjun, Wang, Weimin, Zhao, Wei, Hao, Long. Research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces. JOURNAL OF LOW FREQUENCY NOISE VIBRATION AND ACTIVE CONTROL[J]. 2021, 40(4): 2077-2093, http://apps.webofknowledge.com/CitedFullRecord.do?product=UA&colName=WOS&SID=5CCFccWmJJRAuMzNPjj&search_mode=CitedFullRecord&isickref=WOS:000680723600001.
[6] Zhao, Qingjun, Cui, Weiwei, Xiang, Xiaorong, Xu, Qiangren, Xu, Jianzhong. Numerical investigation of blade tip winglet on flow structure in a high loading transonic rotor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2021, [7] Liu, Zhiyuan, Zhao, Qingjun, Xiang, Xiaorong, Zhao, Wei, Zhou, Xiaoyong. A hybrid viscous body force model for low-speed centrifugal compressors. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2021, 235(3): 335-350, https://www.webofscience.com/wos/woscc/full-record/WOS:000554549600001.
[8] Zhao, Qingjun, Cui, Weiwei, Zhao, Wei, Xiang, Xiaorong, Xu, Jianzhong. Investigation on the effects of winglet geometry in a high loading compressor rotor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2021, 235(8): 1819-1831, http://dx.doi.org/10.1177/09576509211017004.
[9] Sui, Xiuming, Zhao, Wei, Xiang, Xiaorong, Pi, Te, Zhao, Qingjun. Investigation of the flowfield on a vaneless counter-rotating turbine with seal cavity flow ejection. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2021, 235(8): 1864-1876, http://dx.doi.org/10.1177/09576509211018307.
[10] 徐强仁, 刘智远, 项效镕, 周小勇, 赵庆军. 对转压气机外伸激波对叶顶泄漏流影响. 航空动力学报[J]. 2019, 2027-2037, http://lib.cqvip.com/Qikan/Article/Detail?id=72756873504849574857485048.
[11] Kai Zhang, Yingqun Ma, Xiaorong Xiang, Wei Zhao, Qingjun Zhao. Research on Transient Vibration Response of Rotor System Using Supporting Stiffness Active Control. AIAA Propulsion and Energy Forum 2018 Joint Propulsion Conferencenull. 2018, [12] 徐强仁, 马英群, 叶树波, 项效镕, 赵庆军. 高负荷对转压气机尾迹涡级间迁移影响因素研究. 推进技术[J]. 2018, 39(12): 2737-2745, http://lib.cqvip.com/Qikan/Article/Detail?id=6100107587.
[13] Wang, Yunfei, Sui, Xiuming, Zhang, Kai, Xiang, Xiaorong, Zhao, Qingjun. Effects of incidence angle on a low-pressure turbine blade boundary layer evolution through large eddy simulation. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2018, 232(6): 722-734, https://www.webofscience.com/wos/woscc/full-record/WOS:000443311900010.
[14] Zhou, Xiaoyong, Zhao, Qingjun, Xiang, Xiaorong, Cui, Weiwei. Investigation of groove casing treatment in a transonic compressor at different speeds with control volume method. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING[J]. 2016, 230(13): 2392-2408, http://www.corc.org.cn/handle/1471x/2374961.
[15] 黄晨, 项效镕, 张彬彬, 赵巍, 赵庆军. 膨胀式空气涡轮火箭最大状态调节规律与性能分析. 工程热物理学报[J]. 2016, 37(10): 2070-2075, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=5825258&detailType=1.
[16] Cui, Weiwei, Xiang, Xiaorong, Zhao, Qingjun, Xu, Jianzhong. The effect of sweep on flowfields of a highly loaded transonic rotor. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2016, 58: 71-81, https://www.webofscience.com/wos/woscc/full-record/WOS:000388543700007.
[17] Zhang, Binbin, Zhao, Qingjun, Xiang, Xiaorong, Xu, Jianzhong. An improved micro-vortex generator in supersonic flows. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2015, 47: 210-215, http://ir.etp.ac.cn/handle/311046/112318.
[18] 黄晨, 项效镕, 张彬彬, 赵巍, 赵庆军. 基于预冷器特性的膨胀式空气涡轮火箭发动机性能分析. 2015年中国工程热物理学会气动学学术年会null. 2015, http://ir.etp.ac.cn/handle/311046/110974.
[19] Zhao, Qingjun, Zhou, Xiaoyong, Xiang, Xiaorong. Multi-objective optimization of groove casing treatment in a transonic compressor. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY[J]. 2014, 228(6): 626-637, https://www.webofscience.com/wos/woscc/full-record/WOS:000340166200003.
[20] 崔伟伟, 项效镕, 杜建一, 徐建中. 掠效应对高负荷跨音转子性能的影响. 工程热物理学报[J]. 2012, 33(5): 753-756, http://lib.cqvip.com/Qikan/Article/Detail?id=41729095.
[21] 周小勇, 项效镕, 赵庆军. 基于人工神经网络的跨音压气机周向槽机匣处理优化设计. 中国工程热物理学会null. 2012, http://ir.etp.ac.cn/handle/311046/58082.
[22] Bo Liu, Lei Wang, Qingwei Wang, Xiaorong Xiang. Investigation of the Unsteady Flow in an Counter-Rotating Compressor Using the Nonlinear Harmonic Method. ISABEnull. 2011, http://ir.etp.ac.cn/handle/311046/81861.
[23] Liu Bo, Hou Weimin, Nan Xiangyi, Xiang Xiaorong. Numerical and experimental investigation of the dual stage counter rotating compressor by boundary layer suction. ISABEnull. 2009, http://ir.etp.ac.cn/handle/311046/81477.
科研活动
指导学生
已指导学生
徐强仁 博士研究生 080701-工程热物理
现指导学生
张洲 硕士研究生 082502-航空宇航推进理论与工程
任三群 博士研究生 080703-动力机械及工程