Effects of circumferential configuration concerning splitter blade on the aerodynamic performance in

• 作 者: 薛亮 韩万金
• 机 构: PropulsionTheoryandTechnicAcademy
• 出 处: Journal of Harbin Institute of Technology
• 发表日期: 2010年1期
• 关键词: 分流叶片 轴流风机 跨声速 气动性能 圆周 空气动力学性能 配置 数值模拟计算 transonic axial fan splitter blade shock

For a certain type of transonic axial fan, the flow field of a fan rotor with splitter blade was computed by numerical simulation, and the shape of the rotor was modified. The effects of different circumferential distributions concerning the splitter casc