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

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University
China Aviation Industry Corporation

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

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 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.

Original language	English
Pages (from-to)	2445-2448
Number of pages	4
Journal	Science in China, Series E: Technological Sciences
Volume	52
Issue number	8
DOIs	https://doi.org/10.1007/s11431-009-0206-1
State	Published - Aug 2009

Keywords

Asymmetry of wing sweep angle variation
Roll moment
Wing sweep angle

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10.1007/s11431-009-0206-1

Cite this

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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

U2 - 10.1007/s11431-009-0206-1

DO - 10.1007/s11431-009-0206-1

M3 - 文章

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JO - Science in China, Series E: Technological Sciences

JF - Science in China, Series E: Technological Sciences

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

Abstract

Keywords

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