杨策
近期热点
资料介绍
研究领域
1内流流体力学2压缩系统稳定性问题3脉冲膨胀系统非定常流动4燃气轮机技术5增压系统技术"研究项目:负责国家自然科学基金两项负责博士点基金点基金3项负责国防项目7项"近期论文
论文1. Yinhong Liu, Ce Yang, Ben Zhao, Hanzhi Zhang, Mingxu Qi. Geometrical influence on downstream centrifugal impeller inlet distortion in an axial-radial combined compressor[C]. Busan, Korea: 21st ISABE Conference, 2013, No.ISABE-2013-11442. Ben Zhao, Ce Yang, Dazhong Lao, Liangjun Hu, Hanzhi Zhang. Numerical investigation of stator wake oscillation in an axial-radial combined compressor[C]. Busan, Korea: 21st ISABE Conference, 2013, No.ISABE-2013-11293. Hu Liangjun, Sun Harold, Jianwen,Eric Curtis,Anthony Morelli,Jizhong Zhang,Ben Zhao,Ce Yang, Xin Shi, Shangtao Liu. Investigation of Nozzle Clearance Effects on a Radial Turbine: Aerodynamic Performance and Forced Response[C]. SAE Technical Paper, 2013,No.2013-01-09184. WANG Lei-lei, YANG Ce, Zhao Ben, LAO Dazhong, MA Chaochen, LI Du. The Change of the Inlet Geometry of a Centrifugal Compressor Stage and Its Influence on the Compressor Performance[J]. Journal of Thermal Science, 2013, 22(3): 197-2085. Ben Zhao, Ce Yang, Liangjun Hu, Dazhong Lao. Effects of Blade Counts and Clocking on the Unsteady Profile Pressure Distribution in an Axial-Radial Combined Compressor[C]. San Antonio :ASME Turbo Expo,2013,No. GT2013-942516. Ce Yang, Ben Zhao, C C Ma, Dazhong Lao, Mi Zhou. Effect of the Different Geometrical Inlet Pipe on the High Speed Centrifugal Compressor[C]. San Antonio :ASME Turbo Expo,2013,No. GT2013- 942547. Du Li, Dazhong Lao, Ben Zhao, Ce Yang. Stator Wake Research in Axial-Radial Combined Compressor with Inlet Distortion[C]. San Antonio :ASME Turbo Expo,2013, GT2013- 948858. Ben Zhao,Ce Yang*,Shan Chen,Ming-xu Qi,Mi Zhou. Unsteady Flow Variability Driven by Rotor-stator Interaction at Rotor Exit. Chinese Journal of Aeronautics. 25(6):871-878,20129. Islem B,Yang Ce*. Steady Air Injection Flow Control in Centrifugal Compressor. Applied Mechanics and Materials,138-139,471-477,201210. Islem B, Yang Ce*, Li Du, Chen Shan. Steady Air Injection Flow Control for Increasing the Surge Margin of Radial Flow Compressor [J]. Journal of Beijing Institute of Technology, 21(3):321-327,201211. LI Du, YANG Ce*, ZHOU Mi, ZHU Zhifu, WANG Hang. Numerical and Experimental Research on Different Inlet Configurations of High Speed Centrifugal Compressor[J]. Sci China Ser E-Tech Sci, 55(1): 174-181,201212. Islem B, Yang Ce*. Numerical simulation of Steady Air injection flow control effects on a transonic axial flow compressor. Applied Mechanical and Materials, 224:352-357,201213. LI Du, YANG Ce*, ZHAO Ben, ZHOU Mi, QI Mingxu, ZHANG Jizhong. Investigation on Centrifugal Impeller in an Axial-Radial Combined Compressor with Inlet Distortion. Journal of Thermal Science,20(6):486-494,201114. HU Liangjun, YANG Ce*, Sun Harold, ZHANG Jizhong, Lai Mingchia. Numerical Analysis of Nozzle Clearance's Effect on Turbine Performance. Chinese Journal of Mechanical Engineering,24(4):618-625,201115. YANG Ce*, CHEN Shan, Li Du, YANG Changmao, WANG Yidi. Inlet Recirculation Influence to the Flow Structure of Centrifugal Impeller. Chinese Journal of Mechanical Engineering,23(5): 647-654. 201016. Wang Leilei,Yang Ce*. The change of Inlet Geometry of a Centrifugal Compressor Stage and Its Influence on the Compressor Performance. Journal of Thermal Science,201317. Ben Zhao, Ce Yang*, Liangjun Hu, Mi Zhou, Du Li. Investigation of Separating and Utilizing the Influences of Up- and Downstream Blade rows. ASME Paper,2012,GT2012-68371 相关热点