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Effect of forewing sweeping on aerodynamic performance of butterfly like model

Le WANG Gang WANG Bifeng SONG Yang PEI

中国航空学报（英文版）2025，Vol.38Issue(6)：318-335,18.

中国航空学报（英文版）2025，Vol.38Issue(6)：318-335,18.DOI:10.1016/j.cja.2024.103387

Effect of forewing sweeping on aerodynamic performance of butterfly like model

Le WANG ¹Gang WANG ²Bifeng SONG ²Yang PEI²

作者信息

1. School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China
2. School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China||National Key Laboratory of Aircraft Configuration Design,Xi'an 710072,China
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摘要

关键词

Aerodynamics/Butterfly/Immersed boundary method/Adaptive mesh/Micro air vehicles

Key words

Aerodynamics/Butterfly/Immersed boundary method/Adaptive mesh/Micro air vehicles

引用本文复制引用

Le WANG,Gang WANG,Bifeng SONG,Yang PEI..Effect of forewing sweeping on aerodynamic performance of butterfly like model[J].中国航空学报（英文版）,2025,38(6):318-335,18.

基金项目

This research was supported by the National Natural Science Foundation of China(No.52175277).The computations were conducted in Computing Center in Xi'an.The authors thank-fully acknowledge these institutions. （No.52175277）

中国航空学报（英文版）

ISSN：1000-9361

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