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发动机叶栅的实验研究和数值预测

Experimental research and numerical prediction for engine cascades

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【作者】 黄明强朱永波

【Author】 HUANG Ming-qiang, ZHU Yong- bo ( School of Mathematics and Physics, North China Electric Power University, Baoding 071003, China; Research Institute of Beijing Changcheng Aeronautical Measurement and Control Technology, Beijing 100022, China)

【机构】 华北电力大学数理学院北京长城航空测控技术研究所 河北 保定 071003北京 100022

【摘要】 在暂冲式跨音速平面透平叶栅风洞上对某叶栅进行了吹风试验。通过数值预估实验叶栅流场,提供了流场大体结构,设计了实验方案。为选择压力传感器量程和布置测点位置提供了依据。实验测量得到了设计安装角及变工况下叶片表面压力、叶片表面等熵马赫教及波系结构随叶栅进口气流角的变化,并对叶栅内部及出口流场进行了纹影照相。数值预测与试验结果相比较,在大部分情况下,吻合得很好,说明了计算程序的可靠性。反过来,试验结果又可用于检验和改进N.S方程计算程序。

【Abstract】 An air blowing experiment is done on a cascade of a pulse trans-sonic plane turbine cascade tunnel. By the numerical prediction of blade flow field, structure of flow field is proposed and the experimental scheme is designed. This offers the basis for selection of pressure sensor and distribution of measuring points. The designed fixing angle, surface pressure of blade under varing working conditions, the iso-entropy Mach number and the variation of waves structure with air intake’s flow angle are obtained through experiments. Photos of internal blade and outlet Sow field are taken. The numerical prediction results are compared with experimental results. They fit well in most cases. The experimental data can be used to verify and improve the N. S equations program.

【关键词】 透平叶栅N.S方程激波
【Key words】 turbine cascadeN. S equationsshock
  • 【文献出处】 华北电力大学学报 ,Journal of North China Electric Power University , 编辑部邮箱 ,2005年04期
  • 【分类号】TK40
  • 【被引频次】1
  • 【下载频次】100
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