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Space-marching inverse design of subsonic,transonic,and supersonic internal flowfields

Bo ZHANG Shihe YI Yuxin ZHAO Rui YANG Ziyuan ZHU Ruitong ZENG

中国航空学报（英文版）2025，Vol.38Issue(2)：15-30,16.

中国航空学报（英文版）2025，Vol.38Issue(2)：15-30,16.DOI:10.1016/j.cja.2024.05.014

Space-marching inverse design of subsonic,transonic,and supersonic internal flowfields

Bo ZHANG ¹Shihe YI ¹Yuxin ZHAO ¹Rui YANG ¹Ziyuan ZHU ¹Ruitong ZENG¹

作者信息

1. College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410072,China
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摘要

关键词

Flowfield/Inverse design/Compressible flow/Contraction/Nozzle/Asymmetric channel

Key words

Flowfield/Inverse design/Compressible flow/Contraction/Nozzle/Asymmetric channel

引用本文复制引用

Bo ZHANG,Shihe YI,Yuxin ZHAO,Rui YANG,Ziyuan ZHU,Ruitong ZENG..Space-marching inverse design of subsonic,transonic,and supersonic internal flowfields[J].中国航空学报（英文版）,2025,38(2):15-30,16.

基金项目

This research was supported by the National Key Research and Development Program of China(No.2019YFA0405300),and the National Natural Science Founda-tion of China(No.12272405). （No.2019YFA0405300）

中国航空学报（英文版）

ISSN：1000-9361

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