Effect of Wing-Wing Interaction on the Propulsive Performance of Two Flapping Wings at Biplane Configuration

The biplane counter-flapping wing is a special type of wing flapping which is inspired from the fish and insect in nature. The propulsive performance is one of the most important considerations for this kind of flapping wing. This paper is aimed at providing a systematic synthesis on the propulsive...

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Main Authors: Jianyang Zhu, Bin Lei
Format: Article
Language:English
Published: Hindawi Limited 2018-01-01
Series:Applied Bionics and Biomechanics
Online Access:http://dx.doi.org/10.1155/2018/8901067
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spelling doaj-22e313de545941e4951fceec9a5dd2482021-07-02T12:37:20ZengHindawi LimitedApplied Bionics and Biomechanics1176-23221754-21032018-01-01201810.1155/2018/89010678901067Effect of Wing-Wing Interaction on the Propulsive Performance of Two Flapping Wings at Biplane ConfigurationJianyang Zhu0Bin Lei1School of Machinery and Automation, Wuhan University of Science and Technology, Wuhan 430081, ChinaHubei Key Laboratory of Mechanical Transmission and Manufacturing Engineering, Wuhan University of Science and Technology, ChinaThe biplane counter-flapping wing is a special type of wing flapping which is inspired from the fish and insect in nature. The propulsive performance is one of the most important considerations for this kind of flapping wing. This paper is aimed at providing a systematic synthesis on the propulsive characteristics of two flapping wings at biplane configuration based on the numerical analysis approach. Firstly, parameters of this special flapping wing are presented. Secondly, the numerical method for simultaneously solving the incompressible flow and counter-flapping motion of the wing is illustrated, and the method is then validated. Thirdly, the effects of phase angle and mean wing spacing on the propulsive characteristics of the biplane counter-flapping wing are analyzed. Finally, the quantification effects of the phase angle and mean wing spacing on the propulsive characteristics of the biplane counter-flapping wing can be obtained. The analysis results in this study will provide useful guidelines to design an effectively propulsive system applying for the flapping micro air or underwater vehicle.http://dx.doi.org/10.1155/2018/8901067
collection DOAJ
language English
format Article
sources DOAJ
author Jianyang Zhu
Bin Lei
spellingShingle Jianyang Zhu
Bin Lei
Effect of Wing-Wing Interaction on the Propulsive Performance of Two Flapping Wings at Biplane Configuration
Applied Bionics and Biomechanics
author_facet Jianyang Zhu
Bin Lei
author_sort Jianyang Zhu
title Effect of Wing-Wing Interaction on the Propulsive Performance of Two Flapping Wings at Biplane Configuration
title_short Effect of Wing-Wing Interaction on the Propulsive Performance of Two Flapping Wings at Biplane Configuration
title_full Effect of Wing-Wing Interaction on the Propulsive Performance of Two Flapping Wings at Biplane Configuration
title_fullStr Effect of Wing-Wing Interaction on the Propulsive Performance of Two Flapping Wings at Biplane Configuration
title_full_unstemmed Effect of Wing-Wing Interaction on the Propulsive Performance of Two Flapping Wings at Biplane Configuration
title_sort effect of wing-wing interaction on the propulsive performance of two flapping wings at biplane configuration
publisher Hindawi Limited
series Applied Bionics and Biomechanics
issn 1176-2322
1754-2103
publishDate 2018-01-01
description The biplane counter-flapping wing is a special type of wing flapping which is inspired from the fish and insect in nature. The propulsive performance is one of the most important considerations for this kind of flapping wing. This paper is aimed at providing a systematic synthesis on the propulsive characteristics of two flapping wings at biplane configuration based on the numerical analysis approach. Firstly, parameters of this special flapping wing are presented. Secondly, the numerical method for simultaneously solving the incompressible flow and counter-flapping motion of the wing is illustrated, and the method is then validated. Thirdly, the effects of phase angle and mean wing spacing on the propulsive characteristics of the biplane counter-flapping wing are analyzed. Finally, the quantification effects of the phase angle and mean wing spacing on the propulsive characteristics of the biplane counter-flapping wing can be obtained. The analysis results in this study will provide useful guidelines to design an effectively propulsive system applying for the flapping micro air or underwater vehicle.
url http://dx.doi.org/10.1155/2018/8901067
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AT binlei effectofwingwinginteractiononthepropulsiveperformanceoftwoflappingwingsatbiplaneconfiguration
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