Multi-point optimal design for diffuser cascades of centrifugal compressors

被引：8

作者：

Fan, HY ^{[1
]}

Xi, G ^{[1
]}

Wang, SJ ^{[1
]}

机构：

[1] Xian Jiao Tong Univ, Sch Energy & Power Engn, SER Turbomachinery Res Ctr, Xian 710049, Peoples R China

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY | 2000年 / 214卷 / A2期

关键词：

genetic algorithm; centrifugal compressor; cascade; optimal design;

D O I：

10.1243/0957650001538281

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

The 'multi-point design' approach for single airfoils in aeronautical engineering is introduced into the optimal design for diffuser cascades of centrifugal compressors. Genetic algorithms are used to solve the multi-point problem. The proposed approach is applied to a 'two-point design' of a real diffuser cascade. The numerical results show that a group of optimal blade profiles can be obtained, from which the designer can select performance compromises for the two given design condition points.

引用

页码：187 / 190

页数：4

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