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A Phased Aerodynamic Optimization Method for Compressors Based on Multi-Degrees-of-Freedom Surface Parameterization

CHENG Jinxin YANG Chengwu ZHAO Shengfeng

热科学学报（英文版）2021，Vol.30Issue(6)：2071-2086,16.

A Phased Aerodynamic Optimization Method for Compressors Based on Multi-Degrees-of-Freedom Surface Parameterization

CHENG Jinxin ¹YANG Chengwu ²ZHAO Shengfeng¹

作者信息

1. Key Laboratory of Light-duty Gas-turbine,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China
2. School of Aeronautics and Astronautics,University of Chinese Academy of Sciences,Beijing 100049,China
折叠

摘要

关键词

surface parameterization/aerodynamic optimization/compressor blade/phased strategy

Key words

surface parameterization/aerodynamic optimization/compressor blade/phased strategy

引用本文复制引用

CHENG Jinxin,YANG Chengwu,ZHAO Shengfeng..A Phased Aerodynamic Optimization Method for Compressors Based on Multi-Degrees-of-Freedom Surface Parameterization[J].热科学学报（英文版）,2021,30(6):2071-2086,16.

基金项目

This study is financially supported by Civil Aircraft Special Project(Grant No.MJZ-2017-D-32(Y81H061A41)). （Grant No.MJZ-2017-D-32(Y81H061A41）

热科学学报（英文版）

OACSCDEISCI

ISSN：1003-2169

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