首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.6 pt.A; 20050606-09; Reno-Tahoe,NV(US) >SHORT LENGTH-SCALE ROTATING STALL INCEPTION IN A TRANSONIC AXIAL COMPRESSOR - EXPERIMENTAL INVESTIGATION
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SHORT LENGTH-SCALE ROTATING STALL INCEPTION IN A TRANSONIC AXIAL COMPRESSOR - EXPERIMENTAL INVESTIGATION

机译:跨轴压气机的短尺度旋转失速折弯-实验研究

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摘要

To improve the understanding of spike-type stall inception of a transonic axial compressor, measurements of the unsteady static pressure in the rotor endwall region are analyzed. At design speed, a detailed experimental investigation of the unsteadiness of the pressure field at the rotor endwall at near stall condition shows a strong fluctuation of the tip clearance flow. Both vortex strength and -trajectory oscillate randomly. Analysis of the wall pressure time histories during stall inception suggests that spike-type disturbances of the flow field correlate with an upstream motion of one blade passages shock front. In addition, the evolution of a stall cell could be visualized by means of static wall-pressure contour plots.
机译:为了提高对跨音速轴流式压缩机的尖峰型失速开始的理解,分析了转子端壁区域中非稳态静压力的测量值。在设计速度下,在接近失速条件下对转子端壁处压力场的不稳定性进行的详细实验研究表明,叶尖间隙流量存在较大波动。涡流强度和轨迹都随机振荡。对失速开始期间壁压力时间历史的分析表明,流场的尖峰型扰动与一个叶片通道的激波前部的上游运动相关。此外,可以通过静态壁压等高线图可视化失速细胞的演变。

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