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Unsteady pressure field investigation of an axial fan - blade unsteady pressure field measurement

机译:轴流风扇叶片非恒定压力场测量的研究。

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A 1.829 in (6 ft) diameter industrial large flow-rate axial fan operated with 1770 rpm was studied experimentally in laboratory conditions. The flow characteristics near the fan blade surfaces were investigated by measuring the pressure distributions on the blade suction and pressure surfaces and the results were discussed by comparing with analytical formulations. Flow visualizations were also performed to validate the flow characteristics near the blade surface and demonstrated that the flow characteristics near the fan blade surface were dominated by the centrifugal force of the fan rotation, which result in strong three-dimensional flows. The time-dependent pressure measurement showed that the pressure oscillations on the fan blade were significantly dominated by vortex shedding from the fan blades. It was further demonstrated that the pressure distributions during the fan start-up were severely unsteady, and the main frequency variation of the static pressure was much smaller than the fan rotational frequency. The time-dependent pressure measurement when the fan operated at a constant speed showed that the magnitude of the blade pressure variation with time and the main variation frequency was much smaller than the fan rotational frequency. The pressure variations that were related to the vortex shedding were smaller than the fan rotational frequency. The complete set of blade-surface pressure measurements obtained can be used as a guide for performance improvements, vibration analysis, and CFD code validation.
机译:在实验室条件下,通过实验研究了直径为1.829英寸(6英尺)的工业大流量轴流风机,转速为1770 rpm。通过测量叶片吸力和压力表面上的压力分布来研究风扇叶片表面附近的流动特性,并通过与分析公式进行比较来讨论结果。还进行了流动可视化,以验证叶片表面附近的流动特性,并证明风扇叶片表面附近的流动特性受风扇旋转的离心力所控制,从而产生了强劲的三维流动。随时间变化的压力测量结果表明,风扇叶片上的压力振荡主要由风扇叶片上的涡旋脱落所主导。进一步证明,风扇启动过程中的压力分布非常不稳定,并且静压的主频率变化远小于风扇旋转频率。风扇以恒定速度运行时随时间变化的压力测量结果显示,叶片压力随时间变化的幅度和主要变化频率远小于风扇旋转频率。与涡旋脱落有关的压力变化小于风扇旋转频率。获得的完整的叶片表面压力测量值可以用作性能改进,振动分析和CFD代码验证的指南。

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