《Table 4 Ranges of different vane regions》
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《Experimental Investigation on the Effect of Mainstream Turbulence on Full Coverage Film Cooling Effectiveness for a Turbine Guide Vane》
The film cooling performance is different at different regions of the vane surface.To get more comprehensive results,the contour plot is divided into three regions to be discussed:top,mid and down regions.The positions of the three regions are shown in Fig.6(a).The detailed ranges of regions are given in Table 4.The spanwise breadth of each region is about 10%of the vane height.It should be noted that the following discussions of spanwise averaged film cooling effectiveness are based on the three regions.
图表编号 | XD0039674000 严禁用于非法目的 |
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绘制时间 | |
作者 | FU Zhongyi、ZHU Huiren、CHENG Lijian、JIANG Ru |
绘制单位 | School of Power and Energy, Northwestern Polytechnical University、School of Power and Energy, Northwestern Polytechnical University、School of Power and Energy, Northwestern Polytechnical University、School of Power and Energy, Northwestern Polytechnical Un |
更多格式 | 高清、无水印(增值服务) |