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Adjoint-Based Geometrically Constrained Aerodynamic Optimization of a Transonic Compressor Stage

SU Xinrong MA Can YUAN Xin

热科学学报（英文版）2019，Vol.28Issue(5)：850-861,12.

Adjoint-Based Geometrically Constrained Aerodynamic Optimization of a Transonic Compressor Stage

SU Xinrong ¹MA Can ²YUAN Xin¹

作者信息

1. Key Laboratory for Thermal Science and Power Engineering of Ministry of Education, Tsinghua University, Beijing 100084, China
2. Science and Technology on Thermal Energy and Power Laboratory, Wuhan 430205, China
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摘要

关键词

aerodynamic optimization/compressor stage/discrete adjoint method/geometric constraint

Key words

aerodynamic optimization/compressor stage/discrete adjoint method/geometric constraint

引用本文复制引用

SU Xinrong,MA Can,YUAN Xin..Adjoint-Based Geometrically Constrained Aerodynamic Optimization of a Transonic Compressor Stage[J].热科学学报（英文版）,2019,28(5):850-861,12.

基金项目

This work is financially supported by National Natural Science Foundation of China,under project No.51876098 and No.51506107. （）

热科学学报（英文版）

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ISSN：1003-2169

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