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杨金广
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研究员
博士生导师
硕士生导师
- 性别：男
- 毕业院校：西北工业大学
- 学位：博士
- 所在单位：能源与动力学院
- 办公地点：能动楼611
访问量：
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[1] 杨绍文, 杨金广, 王晓放, Ma, Ziyue.A real gas-based throughflow method for the analysis of SCO2 centrifugal compressors[J],PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C JOURNAL OF ME,2022,234(10):1943-1958
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[2] 张敏, 刘艳, 杨金广, Jiang, Xiaowu, 杨绍文, 王晓放.Design and analysis of a multi-stage axial turbine for gasified coal-water power system[J],INTERNATIONAL JOURNAL OF ENERGY RESEARCH,2022,45(5):7352-7365
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[3] 杨金广, 张敏, Peng, Cheng, Ferlauto, Michele, 刘艳.Stator re-stagger optimization in multistage axial compressor[J],PROPULSION AND POWER RESEARCH,2022,10(2):107-117
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[4] Yang, Chen, Wu, Hu, Du, Juan, Zhang, Hongwu, 杨金广.航空发动机部件和整机通流数值模拟研究[J],Journal of Engineering Thermophysics,44(4):894-902
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[5] 张慧颖, 张少杰, 万思远, Liu, Yan, 杨金广, 徐胜利, Wei, Wei.Shape Optimization of Exhaust Volute for a Mixed Working Fluid Centrifugal Compressor[J],International Journal of Gas Turbine, Propulsion and Power Systems,2024,15(4):16-24
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[6] 岳文浩, 师晨月, Yang, Chen, 杨金广, Liao, Naibing.Uncertainty quantification of the inlet boundary conditions in a supercritical CO2 centrifugal compr[J],ENERGY,2024,310
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[7] Wenyang Shao, Juan Du, 杨金广, 王晓放, Guochuan Lyu..Investigation on One-Dimensional Loss Models for Predicting Performance of Multistage Centrifugal Co[J],Journal of Thermal Science,2021,3:133-148
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[8] 杨金广, Zhang, Min, Liu, Yan.NUMERICAL SIMULATIONS AND OPTIMIZATIONS FOR TURBINE-RELATED CONFIGURATIONS[J],THERMAL SCIENCE,2021,24(1):367-378
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[9] Shao, Wenyang, Du, Juan, 杨金广, 王晓放, Lyu, Guochuan.Investigation on One-Dimensional Loss Models for Predicting Performance of Multistage Centrifugal [J],JOURNAL OF THERMAL SCIENCE,2021,30(1):133-148
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[10] Yang, Chen, Wu, Hu, Jin-Guang, Wang, Da-Lei, Jin-Guang(jinguang_yang@dlut.edu.cn).基于时间推进的涡扇发动机整级通流数值模拟[J],推进技术,2019,40(10):2190-2197
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[11] Yang, Chen, Wu, Hu, Jinguang, Ferlauto, Michele, JG (reprint author), Dalian Univ Technol, 2 Linggong Rd, Dalian 116024, Liaoning, Peoples R China..Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade[J],PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF
AEROSPACE ENGINEERING,2019,233(14):5239-5252
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[12] 李志, 刘艳, 杨金广, 徐乐, 张敏, Liu, Yan(yanliu@dlut.edu.cn).超声速涡轮叶型全局气动优化设计[J],推进技术,2018,40(5):1051-1057
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[13] Lv, Guochuan, Wang, Xiaofang, Shao, Wenyang, Yang, Jinguang, XF (reprint author), Dalian Univ Technol, Sch Energy & Power Engn, Dalian 116024, Peoples R China..Aerodynamic design optimization of radial-inflow turbine in supercritical CO2 cycles using a one-d[J],ENERGY CONVERSION AND MANAGEMENT,2018,165:827-839
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[14] 杨金广, 徐乐, 刘艳, 张敏.基于反方法的高负荷涡轮动叶激波控制[J],推进技术,2018,39(6):1240-1249
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[15] 吕国川, 杨金广, 王晓放.超临界二氧化碳向心涡轮设计及变工况性能预测[J],工程热物理学报,2018,39(2):314-320
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[16] 杨金广, 王春雪, 王大磊, 邵伏永, 杨晨, 吴虎, Yang, Jinguang(jinguang_yang@dlut.edu.cn).基于时间推进的通流计算方法:现状及展望[J],航空学报,2017,38(9):58-70
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[17] 杨金广, 张敏, 刘艳, 莫宝玺, Zhang, Min(modest_zm@126.com).环形涡轮动叶栅旋转效应数值研究[J],推进技术,2017,38(10):2280-2289
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[18] Yang, J., Liu, Y., Wu, H., Wang, X., Y (reprint author), Dalian Univ Technol, Sch Energy & Power Engn, Dalian, Peoples R China..An improved steady inverse method for turbomachinery aerodynamic design[J],INVERSE PROBLEMS IN SCIENCE AND ENGINEERING,2017,25(5):633-651
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[19] Yang, Jinguang, Liu, Yan, Wang, Xiaofang, Wu, Hu.3D VISCOUS INVERSE DESIGN OF TURBOMACHINERY USING ONE-EQUATION TURBULENCE MODEL[A],2016,2C-2016
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[20] Shao, Wenyang, Wang, Xiaofang, Yang, Jinguang, Liu, Huimin, Huang, Zhenjun.DESIGN PARAMETERS EXPLORATION FOR SUPERCRITICAL CO2 CENTRIFUGAL COMPRESSORS UNDER MULTIPLE CONSTRA[A],2016,9:383-391
