Flow Calculation in Centrifugal Compressors Using a Quasi-Three-Dimensional Model

被引：1

作者：

Potashev, A., V ^{[1
]}

Potasheva, E., V ^{[1
]}

Hisameev, I. G. ^{[2
]}

机构：

[1] Russian Univ Cooperat, Kazan Cooperat Inst Branch, N Ershova St 58, Kazan, Russia

[2] Kazan Natl Res Technol Univ, K Marx St 68, Kazan, Russia

来源：

OIL AND GAS ENGINEERING (OGE-2020) | 2020年 / 2285卷

基金：

俄罗斯基础研究基金会;

关键词：

flow part of turbomachines; blade elements; calculation and design methods; subsonic gas flow;

D O I：

10.1063/5.0026704

中图分类号：

O69 [应用化学];

学科分类号：

081704 ;

摘要：

When designing centrifugal compressors and turbomachines for various purposes one must carry out the calculation of flow through their fixed and movable elements. One approach to solving this problem is to use the well-proven classical quasi-three-dimensional model. Previously, the authors developed a method for accounting for the compressibility of a gas stream in the flow part of a turbomachine. This article demonstrates the work of a software package compiled on this basis that performs calculations taking into account the mutual influence of the solutions of two two-dimensional problems in the case of a subsonic gas flow.

引用

页数：8