Application of CFD method to achieve the fluid field of an "Infinite Swept Wing" in wind tunnel

Sui Han Zuo; Yong Yang; Dong Li

Application of CFD method to achieve the fluid field of an "Infinite Swept Wing" in wind tunnel

Sui Han Zuo
, Yong Yang
, Dong Li

材料学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

In order to achieve the fluid field of an "Infinite Swept Wing" in a wind tunnel, wall-liners formed from the inviscid streamlines of an infinite swept wing are designed to correct the side wall influence of the wind tunnel. According to CFD results, in a relatively large range in span direction, the flow around the wind tunnel test model is nearly the same as the flow around an infinite swept wing, even with a small aspect ratio.

源语言	英语
页（从-至）	578-581
页数	4
期刊	Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
卷	27
期	5
出版状态	已出版 - 10月 2009

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引用此

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title = "Application of CFD method to achieve the fluid field of an {"}Infinite Swept Wing{"} in wind tunnel",

abstract = "In order to achieve the fluid field of an {"}Infinite Swept Wing{"} in a wind tunnel, wall-liners formed from the inviscid streamlines of an infinite swept wing are designed to correct the side wall influence of the wind tunnel. According to CFD results, in a relatively large range in span direction, the flow around the wind tunnel test model is nearly the same as the flow around an infinite swept wing, even with a small aspect ratio.",

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AU - Yang, Yong

AU - Li, Dong

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N2 - In order to achieve the fluid field of an "Infinite Swept Wing" in a wind tunnel, wall-liners formed from the inviscid streamlines of an infinite swept wing are designed to correct the side wall influence of the wind tunnel. According to CFD results, in a relatively large range in span direction, the flow around the wind tunnel test model is nearly the same as the flow around an infinite swept wing, even with a small aspect ratio.

AB - In order to achieve the fluid field of an "Infinite Swept Wing" in a wind tunnel, wall-liners formed from the inviscid streamlines of an infinite swept wing are designed to correct the side wall influence of the wind tunnel. According to CFD results, in a relatively large range in span direction, the flow around the wind tunnel test model is nearly the same as the flow around an infinite swept wing, even with a small aspect ratio.

KW - CFD method

KW - Infinite swept wing

KW - Wind tunnel testing

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Application of CFD method to achieve the fluid field of an "Infinite Swept Wing" in wind tunnel

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