Design, modal analysis and tests of composites wing box

Bingshan Liu; Ying Yan; Wei Qian; Yuexin Duan

Design, modal analysis and tests of composites wing box

Bingshan Liu^*
, Ying Yan
, Wei Qian
, Yuexin Duan

^*此作品的通讯作者

材料科学与工程学院

Beihang University
China Aviation Industry Corporation

科研成果: 期刊稿件 › 文章 › 同行评审

13 引用（Scopus）

摘要

A scaling-down wing-box model was designed on the basis of structural similarity and manufactured by means of integral-forming of composites for modal analysis and test, by which the similarity of structural dynamics and loading transfer were realized simultaneously. The modal analysis and test were done and their results were in good agreement. This model lays a foundation of the flutter test for high-speed wing in low-speed wind tunnel.

源语言	英语
页（从-至）	1026-1028
页数	3
期刊	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
卷	29
期	11
出版状态	已出版 - 11月 2003

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链接到 Scopus 的出版物

引用此

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title = "Design, modal analysis and tests of composites wing box",

abstract = "A scaling-down wing-box model was designed on the basis of structural similarity and manufactured by means of integral-forming of composites for modal analysis and test, by which the similarity of structural dynamics and loading transfer were realized simultaneously. The modal analysis and test were done and their results were in good agreement. This model lays a foundation of the flutter test for high-speed wing in low-speed wind tunnel.",

keywords = "Composite materials, Manufacturing, Modal analysis, Test, Wing-box",

author = "Bingshan Liu and Ying Yan and Wei Qian and Yuexin Duan",

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AU - Liu, Bingshan

AU - Yan, Ying

AU - Qian, Wei

AU - Duan, Yuexin

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Y1 - 2003/11

N2 - A scaling-down wing-box model was designed on the basis of structural similarity and manufactured by means of integral-forming of composites for modal analysis and test, by which the similarity of structural dynamics and loading transfer were realized simultaneously. The modal analysis and test were done and their results were in good agreement. This model lays a foundation of the flutter test for high-speed wing in low-speed wind tunnel.

AB - A scaling-down wing-box model was designed on the basis of structural similarity and manufactured by means of integral-forming of composites for modal analysis and test, by which the similarity of structural dynamics and loading transfer were realized simultaneously. The modal analysis and test were done and their results were in good agreement. This model lays a foundation of the flutter test for high-speed wing in low-speed wind tunnel.

KW - Composite materials

KW - Manufacturing

KW - Modal analysis

KW - Test

KW - Wing-box

UR - https://www.scopus.com/pages/publications/1542397979

M3 - 文章

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SP - 1026

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JO - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

JF - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

IS - 11

ER -

Design, modal analysis and tests of composites wing box

摘要

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