《Table 2 Grid Sensitivity Analysis for Straight Vane Case》
提示:宽带有限、当前游客访问压缩模式
本系列图表出处文件名:随高清版一同展现
《Effect of Bowed/Leaned Vane on the Unsteady Aerodynamic Excitation in Transonic Turbine》
To explore the ability of different grid setting to simulate the unsteady performance of the transonic turbine stage,four grid cases are modelled in this study.The grid-dependency check is conducted by unsteady numerical simulation on the straight vane model with various numbers of grid nodes ranging from 1.2×106 to7.4×106.In Table 2 the mesh sizes for the stator and rotor passages are listed,and the results of the griddependency check are shown.
图表编号 | XD0039673500 严禁用于非法目的 |
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绘制时间 | |
作者 | LIU Jian、QIAO Weiyang、DUAN Wenhua |
绘制单位 | Turbomachinery Aerodynamics and Acoustics Lab (TAAL), School of Power and Energy, Northwestern Polytechnical University、Turbomachinery Aerodynamics and Acoustics Lab (TAAL), School of Power and Energy, Northwestern Polytechnical University、Turbomachinery |
更多格式 | 高清、无水印(增值服务) |