《Table 1 The parameters of the highest testing point of an annular combustor》
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《Design and application of an air-cooled probe for total pressure measurement at combustor outlet》
The demand to the probe are from a testing project of an annular combustor of a turbofan engine,the parameters of the most severe experiment condition are shown in Table 1.
图表编号 | XD0033680900 严禁用于非法目的 |
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绘制时间 | 2019.01.01 |
作者 | LIU Xupeng、SUN Qi、WANG Xiaoliang、XUE Xiusheng、YIN Dong |
绘制单位 | Shenyang Engine Research Institute,Aero Engine Corporation of China、Shenyang Engine Research Institute,Aero Engine Corporation of China、Shenyang Engine Research Institute,Aero Engine Corporation of China、Shenyang Engine Research Institute,Aero Engine Corp |
更多格式 | 高清、无水印(增值服务) |
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