Lift characteristic of the flapping wing micro air vehicle

Ya Feng Zhang; Bi Feng Song; Chang Sheng Yuan; Guo Ming Ji

Lift characteristic of the flapping wing micro air vehicle

Ya Feng Zhang, Bi Feng Song, Chang Sheng Yuan, Guo Ming Ji

航空学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

3 引用（Scopus）

摘要

In order to exploringly investigate lift mechanism of flapping-wing MAV (Micro Air Vehicle), the lift test of flapping-wing MAV is performed in special micro air vehicle wind tunnel of NPU (Northwestern Polytechnical University). The influences of flapping frequency, wind velocity, angle of attack and camber of flapping-wing on lift characteristic are investigated. The relation between phase-angle of flapping and the magnitude of lift force is investigated. The result of wind tunnel test provides guideline in aircraft design and aerodynamic layout design of flapping-wing MAV.

源语言	英语
页（从-至）	519-522
页数	4
期刊	Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
卷	26
期	4
出版状态	已出版 - 12月 2008

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title = "Lift characteristic of the flapping wing micro air vehicle",

abstract = "In order to exploringly investigate lift mechanism of flapping-wing MAV (Micro Air Vehicle), the lift test of flapping-wing MAV is performed in special micro air vehicle wind tunnel of NPU (Northwestern Polytechnical University). The influences of flapping frequency, wind velocity, angle of attack and camber of flapping-wing on lift characteristic are investigated. The relation between phase-angle of flapping and the magnitude of lift force is investigated. The result of wind tunnel test provides guideline in aircraft design and aerodynamic layout design of flapping-wing MAV.",

keywords = "Flapping-wing, Flapping-wing micro air vehicle, Lift characteristic, Wind tunnel test",

author = "Zhang, {Ya Feng} and Song, {Bi Feng} and Yuan, {Chang Sheng} and Ji, {Guo Ming}",

year = "2008",

month = dec,

language = "英语",

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pages = "519--522",

journal = "Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica",

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AU - Zhang, Ya Feng

AU - Song, Bi Feng

AU - Yuan, Chang Sheng

AU - Ji, Guo Ming

PY - 2008/12

Y1 - 2008/12

N2 - In order to exploringly investigate lift mechanism of flapping-wing MAV (Micro Air Vehicle), the lift test of flapping-wing MAV is performed in special micro air vehicle wind tunnel of NPU (Northwestern Polytechnical University). The influences of flapping frequency, wind velocity, angle of attack and camber of flapping-wing on lift characteristic are investigated. The relation between phase-angle of flapping and the magnitude of lift force is investigated. The result of wind tunnel test provides guideline in aircraft design and aerodynamic layout design of flapping-wing MAV.

AB - In order to exploringly investigate lift mechanism of flapping-wing MAV (Micro Air Vehicle), the lift test of flapping-wing MAV is performed in special micro air vehicle wind tunnel of NPU (Northwestern Polytechnical University). The influences of flapping frequency, wind velocity, angle of attack and camber of flapping-wing on lift characteristic are investigated. The relation between phase-angle of flapping and the magnitude of lift force is investigated. The result of wind tunnel test provides guideline in aircraft design and aerodynamic layout design of flapping-wing MAV.

KW - Flapping-wing

KW - Flapping-wing micro air vehicle

KW - Lift characteristic

KW - Wind tunnel test

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M3 - 文章

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SN - 0258-1825

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JO - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

JF - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

IS - 4

ER -

Lift characteristic of the flapping wing micro air vehicle

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