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Automatic and Rapid Throughflow-Based Optimal Design Method for Multi-Stage Axial-Flow Compressors

LEI Fan ZHANG Xiawen JU Yaping ZHANG Chuhua

热科学学报（英文版）2025，Vol.34Issue(1)：77-91,15.

热科学学报（英文版）2025，Vol.34Issue(1)：77-91,15.DOI:10.1007/s11630-024-2005-1

Automatic and Rapid Throughflow-Based Optimal Design Method for Multi-Stage Axial-Flow Compressors

LEI Fan ¹ZHANG Xiawen ²JU Yaping ²ZHANG Chuhua³

作者信息

1. Department of Fluid Machinery and Engineering,School of Energy and Power Engineering,Xi'an Jiaotong University,Xi'an 710049,China||Production and Environmental Department,China Huaneng Group.,Co.,Ltd.,Beijing 100031,China
2. Department of Fluid Machinery and Engineering,School of Energy and Power Engineering,Xi'an Jiaotong University,Xi'an 710049,China
3. Department of Fluid Machinery and Engineering,School of Energy and Power Engineering,Xi'an Jiaotong University,Xi'an 710049,China||State Key Laboratory for Strength and Vibration of Mechanical Structures,Xi'an Jiaotong University,Xi'an 710049,China
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摘要

关键词

multi-stage axial-flow compressor/throughflow design/empirical correlations/genetic algorithm/aerodynamic optimization

Key words

multi-stage axial-flow compressor/throughflow design/empirical correlations/genetic algorithm/aerodynamic optimization

引用本文复制引用

LEI Fan,ZHANG Xiawen,JU Yaping,ZHANG Chuhua..Automatic and Rapid Throughflow-Based Optimal Design Method for Multi-Stage Axial-Flow Compressors[J].热科学学报（英文版）,2025,34(1):77-91,15.

基金项目

This work is financially supported by the National Science and Technology Major Project of China(Grant No.2017-Ⅱ-0006-0020),National Key Research and Development Project of China(Grant No.2016YFB0200901),National Natural Science Foundation of China(Grant No.51776154)and Shaanxi Key Research and Development Project(Grant No.2018KWZ-01). （Grant No.2017-Ⅱ-0006-0020）

热科学学报（英文版）

ISSN：1003-2169

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