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Methods of calculating loading factor characteristic of a centrifugal compressor impeller

机译:离心式压缩机叶轮的负载因子特性计算方法

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Loading factor at design point is calculated by one or other empirical formula in classical design methods. The problem of the whole loading factor performance modeling was out of consideration. Test data on compressor stages demonstrate that loading factor function versus flow coefficient at an impeller exit is of linear character independent of compressibility. Known Universal modeling method exploits this fact. Two points establish the function - loading factor at design point and at zero flow rate. The proper formulae include empirical coefficients. Good result of modeling is possible if choice of the coefficient is based on experience and close analogs. Earlier Y. Galerkin and K. Soldatova have proposed to define a loading factor performance by the angle of its inclination to the ordinate axis and by the loading factor at zero flow rate. Simple and definite equations with four geometry parameters were proposed for loading factor performances calculated for non-viscid flow. The authors of this publication have studied test performances of fifteen stages of different type and ways of modeling. The equations are proposed with universal empirical coefficients. The calculation error lies in the range 1,5% of a loading factor at a design point. The alternative model of a loading factor performance modeling is included in new versions of the Universal modeling method.
机译:设计点的装载因子由经典设计方法中的一个或其他经验公式计算。整个装载因子性能建模的问题是不考虑的。关于压缩机阶段的测试数据表明,叶轮出口处的加载因子函数与流量系数相对于可压缩性无关。已知的普遍建模方法利用这一事实。两个点在设计点和零流量下建立功能 - 装载因子。适当的公式包括经验系数。如果系数的选择基于经验和关闭类似物,则建模的良好结果是可能的。早期的Y. Galerkin和K. Soldatova已经提出通过将装载因子性能定义为纵坐标轴的角度和零流量的装载因子。提出了具有四个几何参数的简单且明确的方程,用于加载用于非粘性流量的因子性能。本出版物的作者研究了对不同类型的十五个阶段的测试表演和建模方式。通过通用经验系数提出了方程。计算误差位于设计点的加载因子的1.5%范围内。装载因子性能建模的替代模型包括在通用建模方法的新版本中。

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