基本信息
耿少娟 女 硕导 中国科学院工程热物理研究所
电子邮件: gengsj@iet.cn
通信地址: 北京北四环西路11号
邮政编码: 100190
电子邮件: gengsj@iet.cn
通信地址: 北京北四环西路11号
邮政编码: 100190
研究领域
1、压气机气动热力学,包括压气机气动设计、流动分析和实验研究等
2、叶轮机械气动声学
招生信息
招生专业
080703-动力机械及工程082502-航空宇航推进理论与工程080704-流体机械及工程
招生方向
压气机气动热力学
教育背景
2002-09--2007-08 中科院工程热物理研究所 工学博士1998-09--2002-07 西安交通大学能源与动力工程学院 工学学士
工作经历
工作简历
2015-08~2016-07,加拿大蒙特利尔工学院 机械工程系, 访问学者2012-09~2012-12,英国斯特莱斯克莱德大学 机械与航空工程系, 访问学者2008-01~现在, 中科院工程热物理研究所, 助理研究员、副研究员
出版信息
发表论文
[1] Li, Xinlong, Jin, Yun, Liu, Shuaipeng, Geng, Shaojuan, Zhang, Xiaoyu, Zhang, Hongwu. Design Optimization of 1.5-Stage Transonic Compressor Based on BPNN Surrogate Model and NSGA-II. MACHINES[J]. 2023, 11(6): http://dx.doi.org/10.3390/machines11060631.[2] Liu, Shuaipeng, Geng, Shaojuan, Li, Xinlong, Jin, Yun, Zhang, Hongwu. Optimization Design of Aspect Ratio and Solidity of a Heavy-Duty Gas Turbine Transonic Compressor Rotor. MACHINES[J]. 2023, 11(1): http://dx.doi.org/10.3390/machines11010082.[3] Jin Yun, Geng Shaojuan, Liu Shuaipeng, Ni Ming, Zhang Hongwu. Design Optimization and Analysis of Exit Rotor with Diffuser Passage based on Neural Network Surrogate Model and Entropy Generation Method. Journal of Thermal Science[J]. 2023, 32(2): 739-752, [4] 刘帅鹏, 耿少娟, 李鑫龙, 金芸, 张宏武. Optimization Design of Aspect Ratio and Solidity of Heavy-Duty Gas Turbine Transonic Compressor Rotor. Machines[J]. 2023, 11(1): 82-, [5] 李鑫龙, 刘帅鹏, 耿少娟, 张宏武. Influence of Hub Contouring on the Performance of a Transonic Axial Compressor Stage with Low Hub-Tip Ratio. Journal of Thermal Science[J]. 2022, 31(1): 179-188, [6] 金芸, 耿少娟, 刘帅鹏, 张宏武. Design Optimization of Exit stage with Diffuser Passage based on NSGA-Ⅱ and Kriging Surrogate Model. The First International Conference on Mechanical System Dynamicsnull. 2022, [7] 金芸, 耿少娟, 王文涛, 张小玉, 张宏武. 多级轴流压气机出口级转子扩张通道优化设计. 航空动力学报[J]. 2022, 37(4): 815-825, http://lib.cqvip.com/Qikan/Article/Detail?id=7107261528.[8] Li Xinlong, Liu Shuaipeng, Geng Shaojuan, Zhang Hongwu. Influence of Hub Contouring on the Performance of a Transonic Axial Compressor Stage with Low Hub-Tip Ratio. JOURNAL OF THERMAL SCIENCE[J]. 2022, 31(1): 179-188, http://apps.webofknowledge.com/CitedFullRecord.do?product=UA&colName=WOS&SID=5CCFccWmJJRAuMzNPjj&search_mode=CitedFullRecord&isickref=WOS:000742926200018.[9] 耿少娟, 张小玉, 丁林超, 王文涛, 卞祥德, 石书成. 转子叶片加工误差对1.5级跨声速压气机气动性能的影响. 推进技术[J]. 2021, 42(1): 139-148, http://lib.cqvip.com/Qikan/Article/Detail?id=7104247009.[10] Li, Jichao, Du, Juan, Geng, Shaojuan, Li, Fan, Zhang, Hongwu. Tip air injection to extend stall margin of multi-stage axial flow compressor with inlet radial distortion. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2020, 96: 105554-, http://dx.doi.org/10.1016/j.ast.2019.105554.[11] Ni Ming, Geng Shaojuan, Wei Zuojun, Gan Xiaohua. A Numerical Study on the Effect of Inter-Stage Water Injection in an Opposed-Setting-Two-Stage Centrifugal Compressor. ASME Turbo Expo 2020: Turbomachinery Technical Conference and Expositionnull. 2020, [12] 倪明, 耿少娟, 张小玉, 张宏武. 空气湿度对舰用燃气轮机两级对置式离心压气机性能的影响. 舰船科学技术[J]. 2020, 42(10): 8-117, https://kns.cnki.net/KCMS/detail/detail.aspx?dbcode=CJFQ&dbname=CJFDAUTODAY&filename=JCKX202019023&v=MTgxODhITkhOcG85SFo0UjhlWDFMdXhZUzdEaDFUM3FUcldNMUZyQ1VSN3FlWnVkdUZ5N25VcjNNTHk3QWRyRzQ=.[13] Li, Jichao, Geng, Shaojuan, Du, Juan, Zhang, Hongwu, Nie, Chaoqun. Circumferentially propagating characteristic dominated by unsteady tip leakage flow in axial flow compressors. AEROSPACE SCIENCE AND TECHNOLOGY[J]. 2019, 85: 529-543, http://dx.doi.org/10.1016/j.ast.2018.11.058.[14] 倪明, 耿少娟, 张宏武, 王永生. 两级对置式离心压气机湿压缩研究. 推进技术[J]. 2019, 41(5): 1000-1014, http://lib.cqvip.com/Qikan/Article/Detail?id=7101985961.[15] 耿少娟, 倪明, 丁林超, 王文涛, 张小玉. 两级双转子对置式离心压气机气动设计和强度校核. 中国舰船研究[J]. 2019, 14(4): 111-119, http://lib.cqvip.com/Qikan/Article/Detail?id=7002688271.[16] 胡开南, 耿少娟, 张宏武. 基于二维紧凑型四阶格子模型的激波管流动模拟. 航空动力学报[J]. 2017, 32(11): 2777-2783, http://lib.cqvip.com/Qikan/Article/Detail?id=674633255.[17] 胡开南, 张宏武, 耿少娟. 可以恢复Navier-Stokes方程的3阶格子Boltzmann作用力模型. 航空动力学报[J]. 2017, 32(8): 1943-1949, http://lib.cqvip.com/Qikan/Article/Detail?id=673807671.[18] 杜娟, 王偲臣, 李继超, 耿少娟, 聂超群. 轴流压气机叶顶泄漏流与突尖先兆失稳机理的研究进展. 推进技术[J]. 2017, 38(10): 2208-2217, http://lib.cqvip.com/Qikan/Article/Detail?id=674625265.[19] 王子楠, 耿少娟, 张宏武. 来流边界层对压气机平面叶栅角区流动的影响. 推进技术[J]. 2017, 38(1): 54-60, https://d.wanfangdata.com.cn/periodical/tjjs201701008.[20] 高磊, 王子楠, 耿少娟, 张宏武, 聂超群. 粗糙度对压气机叶栅损失特性影响的实验研究. 推进技术[J]. 2016, 37(7): 1263-1270, https://d.wanfangdata.com.cn/periodical/tjjs201607009.[21] 王文涛, 王子楠, 耿少娟, 张宏武. 叶栅倒角对压气机角区流动影响的数值模拟和实验研究. 工程热物理学报[J]. 2016, 37(5): 957-962, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=5703944&detailType=1.[22] 王子楠, 耿少娟, 张宏武. 间隙变化对压气机静叶叶栅气动性能的影响. 航空学报[J]. 2016, 37(11): 3304-3316, http://lib.cqvip.com/Qikan/Article/Detail?id=670711989.[23] 白冰, 耿少娟, 李继超, 张宏武, 聂超群. 间隙和转速对轴流压气机非定常叶顶泄漏流周向传播特性影响的实验研究. 工程热物理学报[J]. 2016, 37(7): 1404-1410, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=5743360&detailType=1.[24] Hu, Kainan, Zhang, Hongwu, Geng, Shaojuan. Decoupled scheme based on the Hermite expansion to construct lattice Boltzmann models for the compressible Navier-Stokes equations with arbitrary specific heat ratio. PHYSICAL REVIEW E[J]. 2016, 94(4): 043314-, https://www.webofscience.com/wos/woscc/full-record/WOS:000388438400020.[25] 李继超, 白冰, 耿少娟, 聂超群. 轴流压气机叶顶间隙泄漏流的周向传播特性实验研究. 工程热物理学报[J]. 2015, 36(12): 2599-2603, [26] 赵龙, 耿少娟, 张宏武. 压气机二维动叶栅非定常流场的大涡模拟. 航空动力学报[J]. 2015, 30(1): 248-256, http://sciencechina.cn/gw.jsp?action=detail.jsp&internal_id=5354264&detailType=1.[27] 王子楠, 高磊, 耿少娟, 张宏武. 不同端壁间隙下压气机平面叶栅角区流动的数值模拟和实验研究. 工程热物理学报[J]. 2015, 36(7): 1428-1432, https://d.wanfangdata.com.cn/periodical/gcrwlxb201507009.[28] 张小玉, 耿少娟, 张宏武. 基于目标压力分布的压气机叶型黏性反问题设计方法. 汽轮机技术[J]. 2014, 56(4): 241-245, http://lib.cqvip.com/Qikan/Article/Detail?id=662133256.[29] 刘红蕊, 耿少娟, 方杭安, 聂超群. 对旋式轴流风机变转速匹配性能研究. 机械设计与制造[J]. 2012, 116-118, http://lib.cqvip.com/Qikan/Article/Detail?id=41196491.[30] Geng, S J, Chen, N X, Zhang, H W, Huang, W G. An Improvement on the Efficiency of a Single Rotor Transonic Compressor by Reducing the Shock Wave Strength on the Blade Suction Surfaces. JOURNAL OF THERMAL SCIENCE[J]. 2012, 21(2): 127-135, http://lib.cqvip.com/Qikan/Article/Detail?id=40970178.[31] 耿少娟, 张小玉, 聂超群, 黄伟光, 张宏武. 轴流压气机叶顶端区流场周向传播特征及其预测. 机械工程学报[J]. 2012, 48(16): 130-138, http://lib.cqvip.com/Qikan/Article/Detail?id=43337584.[32] 刘红蕊, 耿少娟, 聂超群, 方杭安. 对旋式轴流风机变环量流型的改进设计. 风机技术[J]. 2011, 34-38, http://lib.cqvip.com/Qikan/Article/Detail?id=38359070.[33] Geng, Shaojuan, Lin, Feng, Chen, Jingyi, Nie, Chaoqun. Evolution of Unsteady Flow near Rotor Tip during Stall Inception. JOURNAL OF THERMAL SCIENCE[J]. 2011, 20(4): 294-303, http://lib.cqvip.com/Qikan/Article/Detail?id=38381225.[34] 黄俊雄, 耿少娟, 吴瑞, 刘克, 聂超群, 张宏武. 不同叶轮形式下离心泵噪声特性对比研究. 声学学报[J]. 2010, 35(2): 113-118, http://lib.cqvip.com/Qikan/Article/Detail?id=33097203.[35] 吴瑞, 冯涛, 耿少娟, 刘克, 聂超群. 一种基于声相似律的旋转流体机械噪声声源分离方法. 声学学报[J]. 2010, 119-125, http://lib.cqvip.com/Qikan/Article/Detail?id=33097204.[36] 耿少娟, 林峰, 张宏武, 黄伟光. 低速单转子轴流压气机突尖型失速特征. 工程热物理学报[J]. 2010, 929-932, http://lib.cqvip.com/Qikan/Article/Detail?id=33998327.[37] Shaojuan Geng, Feng Lin, Jingyi Chen, Hongwu Zhang, Lei He. Circumferential propagation of tip leakage flow unsteadiness for a low-speed axial compressor. JOURNAL OF THERMAL SCIENCE,[J]. 2009, 18(3): 202-206, http://ir.etp.ac.cn/handle/311046/106437.[38] 耿少娟, 张宏武, 陈静宜, 黄伟光. 跨音速轴流压气机叶顶间隙泄漏流对微喷气的非定常响应机制和扩稳效果研究. 工程热物理学报[J]. 2009, 2013-2016, http://lib.cqvip.com/Qikan/Article/Detail?id=32473522.[39] Huang, Weiguang, Geng, Shaojuan, Zhu, Junqiang, Zhang, Hongwu. Numerical simulation of rotating stall in a centrifugal compressor with vaned diffuser. JOURNAL OF THERMAL SCIENCE[J]. 2007, 16(2): 115-120, http://lib.cqvip.com/Qikan/Article/Detail?id=24460663.[40] 耿少娟, 张宏武, 朱俊强, 黄伟光. 喷气对低速轴流压气机转子叶顶区域流动的影响. 工程热物理学报[J]. 2007, 28(3): 395-398, http://lib.cqvip.com/Qikan/Article/Detail?id=24275647.[41] Nie, Chaoqun, Tong, Zhiting, Geng, Shaojuan, Zhu, Junqiang, Huang, Weiguang. Experimental investigations of micro air injection to control rotating stall. JOURNAL OF THERMAL SCIENCE[J]. 2007, 16(1): 1-6, http://lib.cqvip.com/Qikan/Article/Detail?id=24122506.[42] Geng, Shaojuan, Zhang, Hongwu, Chen, Jingyi, Huang, Weiguang. Unsteady tip clearance flow pattern in an isolated axial compressor rotor with micro tip injection. JOURNAL OF THERMAL SCIENCE[J]. 2007, 16(4): 309-320, http://lib.cqvip.com/Qikan/Article/Detail?id=25746180.[43] 耿少娟, 聂超群, 黄伟光, 冯涛, 刘克. 不同叶轮形式下离心泵整机非定常流场的数值研究. 机械工程学报[J]. 2006, 42(5): 27-31, http://lib.cqvip.com/Qikan/Article/Detail?id=21960814.[44] 耿少娟, 朱俊强, 戴冀, 黄伟光. 叶尖喷气影响低速离心压气机特性的数值分析. 工程热物理学报[J]. 2006, 27(3): 411-413, http://www.irgrid.ac.cn/handle/1471x/677552.[45] 戴冀, 耿少娟, 黄伟光. 离心压气机顶部进口条件对叶轮内部流动的影响. 工程热物理学报[J]. 2005, 26(5): 755-757, http://lib.cqvip.com/Qikan/Article/Detail?id=20099634.[46] 耿少娟, 戴冀, 张宏武, 黄伟光. 低速离心压气机的全工况数值模拟和校核. 工程热物理学报[J]. 2005, 81-84, http://lib.cqvip.com/Qikan/Article/Detail?id=1000258491.
科研活动
科研项目
( 1 ) 多叶片通道环境下压气机端区非定常流动的跨通道传播特性, 主持, 国家级, 2010-01--2012-12( 2 ) 风扇压气机非定常流动的控制途径基础研究, 参与, 国家级, 2008-01--2011-12( 3 ) 风扇/压气机动叶端区复杂流动结构、非定常激励与失稳调控的基础研究, 参与, 国家级, 2011-01--2013-12( 4 ) 燃气轮机的高性能热-功转换科学技术问题研究, 参与, 国家级, 2007-07--2011-11( 5 ) CXJJ-16S035, 主持, 部委级, 2016-01--2018-12( 6 ) KGFZD-135-16-019, 主持, 部委级, 2016-01--2018-12( 7 ) 舰船燃机压气机全工况流动机理、气动设计方法及试验验证, 参与, 国家级, 2018-08--2023-07( 8 ) 典型功能器件微纳结构激光制造应用开发, 参与, 国家级, 2018-05--2021-04( 9 ) 1.5级跨音压气机流动机理及实验验证, 主持, 国家级, 2018-08--2023-07
参与会议
(1)多级轴流压气机末级扩张通道设计与研究 中国工程热物理学会热机气动热力学和流体机械学术会议 2020-10-24(2)A NUMERICAL STUDY ON THE EFFECT OF INTER-STAGE WATER INJECTION IN AN OPPOSED-SETTING-TWO-STAGE CENTRIFUGAL COMPRESSOR 3. Ming Ni, Shaojuan Geng, Zuojun Wei, Xiaohua Gan 2020-09-21(3)1.5级跨音压气机气动特性的数值模拟研究 中国工程热物理学会热机气动热力学和流体机械学术会议 2019-10-20(4)The Wet Compression Effect on An Opposed-Setting-Two-Stage Centrifugal Compressor Ni Ming , Geng Shaojuan and Zhang Hongwu 2018-08-22(5)Experimental Study of Circumferential Propagation Features Induced by Unsteady Tip Leakage Flow in Axial Compressor 2017-01-16(6)Tip Leakage Flow Unsteadiness and its Propagation Features in Axial Compressor: Effect of Inlet Hub Distortion 2015-07-13(7)Circumferential Propagation Characteristic in the Blade Tip Region of an Axial Flow Compressor 2015-07-13(8)Numerical Investigation on Interaction between Hub Clearance Flow and Corner Separation in a Planar Compressor Cascade 2014-08-18(9)Numerical Study of Surface Roughness Effects on Compressor Cascade Performance 2014-08-18(10)Evolution of Pressure Signature Dominated by Unsteady Tip Leakage Flow 2013-06-03(11)An Improvement on the Efficiency of a Single Rotor Transonic Compressor by Reducing the Shock Wave Strength on the Blade Suction Surfaces Shaojuan Geng, Naixing Chen, Hongwu Zhang, Weiguang Huang 2011-07-04(12)Evolution of Unsteady Flow near Rotor Tip during Stall Inception 23. Shaojuan Geng, Feng Lin, Jingyi Chen, Chaoqun Nie 2011-07-04