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Parametric study of centrifugal compressor stage vane diffuser characteristics by CFD methods

机译:CFD方法的离心压缩机级叶片漫射特性的参数研究

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The paper presents results of CFD simulations of a series of centrifugal compressor stage vane diffusers in the Ansys CFX. Objects of research are vane diffusers with external relative diameter (relative to the diameter of the impeller) equal to 1.5, vane inlet angles of 15, 20, 25 and 30 degrees, relative vane heights of 0.025, 0.045, 0.06, 0.08, vane profile curvature angles of 10, 15, 20 degrees. The characteristics of the polytropic efficiency, the loss coefficient, the recovery coefficient, the inlet-outlet velocity ratio, the flow deviation angle depending on the incidence angle are calculated. The analysis of the flow pattern in the intervane channel is presented. Increasing the vane curvature angle leads to a diffuser characteristics shift to the area of negative incidence angles. The flow deviation angle is almost independent of the diffuser width and increases with the curvature angle. In most calculations, a narrow diffuser (0.025) shows higher values of characteristics in the area of positive incidence angles. Characteristics of diffusers with a large inlet angle (25-30°) do not have a strong maximum.
机译:本文介绍了ANSYS CFX中一系列离心压缩机级叶片扩散器的CFD模拟的结果。研究对象是具有外部相对直径的叶片扩散器(相对于叶轮的直径)等于1.5,叶片入口角为15,20,25和30度,相对叶片高度为0.025,0.045,0.06,0.08,叶片轮廓曲率角为10,15,20度。计算多细胞效率,损耗系数,回收系数,入口出口速度比,根据入射角的流量偏差角度。介绍了静止信道中的流动模式的分析。增加叶片曲率角度导致漫射器特性转移到负射角区域。流动偏差角几乎与漫射宽度无关,并随着曲率角度增加。在大多数计算中,窄的漫射器(0.025)表示正入射角的区域中的较高值。具有大的入口角度(25-30°)的漫射器的特性没有最大的最大值。

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