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个人简介

教育经历 2009.9 -- 2013.4 西北工业大学 航空宇航推进理论与工程 博士 2004.9 -- 2007.2 中国航天三院 航空宇航推进理论与工程 硕士 2000.9 -- 2004.7 西北工业大学 航空宇航推进理论与工程 学士 社会兼职 北京动力机械研究所特聘专家 《推进技术》第15、16、17届编委

研究领域

叶轮机械气动热力学

近期论文

查看导师新发文章 (温馨提示:请注意重名现象,建议点开原文通过作者单位确认)

Wenyang Shao.Investigation on One-Dimensional Loss Models for Predicting Performance of Multistage Centrifugal Co[J],Journal of Thermal Science,2021,3:133-148 杨金广.NUMERICAL SIMULATIONS AND OPTIMIZATIONS FOR TURBINE-RELATED CONFIGURATIONS[J],THERMAL SCIENCE,2021,24(1):367-378 Shao, Wenyang.Investigation on One-Dimensional Loss Models for Predicting Performance of Multistage Centrifugal [J],JOURNAL OF THERMAL SCIENCE,2021,30(1):133-148 Yang, Chen,Wu, Hu,Yang, Jin-Guang,Wang, Da-Lei.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 Yang, Chen,Wu, Hu,Yang, Jinguang,Ferlauto, Michele.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 李志,刘艳,杨金广,徐乐,张敏.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 Lu, Yeming,Yang, Jinguang,Wang, Xiaofang,Zhou, Fangming.A symmetrical-nonuniform angular repartition strategy for the vane blades to improve the energy co[J],NUCLEAR ENGINEERING AND DESIGN,2018,337:245-260 丛庆丰,姜晓武,杨金广,谢蓉.轴流涡轮准一维性能分析方法研究[A],2018,8 郭莹,杨海军,马利锦,吴辉霞,杨金广.合成氨装置二段炉烧嘴原料改变的性能影响及设计优化[A],2018 Lv, Guochuan,Yang, Jinguang,Shao, Wenyang,Wang, Xiaofang.Aerodynamic design optimization of radial-inflow turbine in supercritical CO2 cycles using a one-d[J],ENERGY CONVERSION AND MANAGEMENT,2018,165:827-839 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 陈节贵,彭铖,杨金广,徐宝鹏.带可调进口导叶的多级轴流压气机非设计点性能计算[J],热科学与技术,2018,17(1):73-79 杨金广,Mechele Ferlauto,Jiri Blazek.Characteristic-Based Formulation of Boundary Conditions for Preconditioned or Non-Preconditioned Flo[A],2018 Michele Ferlauto,Andrea Giuliano,杨金广.Reduced Order Modeling of Thermal Transients in High-Performance Engineering Systems[A],2018 Amin Khan,Michele Ferlauto,杨金广.A Fault/Failure Detection Algorithm based on a Grid of Virtual Sensors for Engine Health Monitoring[A],2018 程中林,谢蓉,杨金广,张靖旋.基于S1 流面的叶轮机械准三维流动计算程序开发[A],2018 吕国川,杨金广,王晓放,祝畅,姜玉雁,郭朝红.MW 级超临界二氧化碳向心涡轮设计及分析[A],2018 徐乐,杨金广,刘艳.基于S1流面粘性反问题的带分流叶片离心叶轮叶片反设计[A],2018 王继磊,杨金广,刘艳.小流量向心涡轮多目标优化设计[A],2018 从庆丰,姜晓武,杨金广,谢蓉.轴流涡轮准一维性能分析方法研究[A],2018 王继磊,杨金广,刘艳,张天宸.Multi-objective optimization design of a centrifugal impeller[A],2018 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 杨金广,王春雪,王大磊,邵伏永,杨晨,吴虎.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 杨金广,张敏,刘艳,莫宝玺.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 Yang, J.,Liu, Y.,Wu, H.,Wang, X..An improved steady inverse method for turbomachinery aerodynamic design[J],INVERSE PROBLEMS IN SCIENCE AND ENGINEERING,2017,25(5):633-651 杨金广,王晓放.基于流线曲率法的多级离心压缩机通流计算[A],2017 王巍,王晓放,杨金广.超临界水煤气化工艺动力循环的设计与性能分析[A],2017 谢蓉,杨金广.一种无壁面距离的SA湍流模型的求解方法[A],2017 Yang, Jinguang,Liu, Yan,Wang, Xiaofang,Wu, Hu.3D VISCOUS INVERSE DESIGN OF TURBOMACHINERY USING ONE-EQUATION TURBULENCE MODEL[A],2016,2C-2016 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 杨金广,王晓放.能量基损失模型于SCO2离心压缩机性能预测有效性研究[A],2016 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[A],2016 刘艳,杨金广.动叶叶顶结构对1.5级涡轮气动性能影响的数值研究[A],2016 杨金广,刘艳.基于一维方法的轴流压气机喘振边界预测模型对比研究[A],2016 杨金广,刘艳.基于S1流面粘性反问题的离心压缩机叶轮改型设计[A],2016 Zhao, Peng-Fei,Liu, Yan,Li, Hong-Kun,Wang, Xiao-Fang,Yang, Jin-Guang.The effect of impeller-diffuser interactions on diffuser performance in a centrifugal compressor[J],ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS,2016,10(1):565-577 王晓放,杨金广.小流量超临界二氧化碳压缩机叶轮设计[A],2015 刘艳,杨金广.涡轮叶栅叶顶间隙泄漏流动及控制研究进展[A],2015

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