The effect of leading-edge sweep angle asymmetry on lateral aerodynamics

Jingxia Zhan; Jinjun Wang

doi:10.1007/s11431-009-0206-1

The effect of leading-edge sweep angle asymmetry on lateral aerodynamics

Jingxia Zhan^*
, Jinjun Wang

^*此作品的通讯作者

航空科学与工程学院

Beihang University
China Aviation Industry Corporation

科研成果: 期刊稿件 › 文章 › 同行评审

4 引用（Scopus）

摘要

Based on the results of force measurement experiment in a low speed wind tunnel, the effect of asymmetrical leading-edge sweep angle on aerodynamic load was investigated with the common-swift's wing model. The wing model was divided into three segments, i.e., arm wing, hand wing_in and hand wing _out, and the roll moment produced by the variation of asymmetrical change of wing segment's leading-edge sweep angle was analyzed.

源语言	英语
页（从-至）	2445-2448
页数	4
期刊	Science in China, Series E: Technological Sciences
卷	52
期	8
DOI	https://doi.org/10.1007/s11431-009-0206-1
出版状态	已出版 - 8月 2009

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10.1007/s11431-009-0206-1

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title = "The effect of leading-edge sweep angle asymmetry on lateral aerodynamics",

abstract = "Based on the results of force measurement experiment in a low speed wind tunnel, the effect of asymmetrical leading-edge sweep angle on aerodynamic load was investigated with the common-swift's wing model. The wing model was divided into three segments, i.e., arm wing, hand wingin and hand wing out, and the roll moment produced by the variation of asymmetrical change of wing segment's leading-edge sweep angle was analyzed.",

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AB - Based on the results of force measurement experiment in a low speed wind tunnel, the effect of asymmetrical leading-edge sweep angle on aerodynamic load was investigated with the common-swift's wing model. The wing model was divided into three segments, i.e., arm wing, hand wingin and hand wing out, and the roll moment produced by the variation of asymmetrical change of wing segment's leading-edge sweep angle was analyzed.

KW - Asymmetry of wing sweep angle variation

KW - Roll moment

KW - Wing sweep angle

UR - https://www.scopus.com/pages/publications/67650770182

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The effect of leading-edge sweep angle asymmetry on lateral aerodynamics

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