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Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle

Inspired by superior flight performance of natural flight masters like birds and insects and based on the ventilating flaps that can be opened and closed by the changing air pressure around the wing, a new flapping wing type has been proposed. It is known that the net lift force generated by a solid...

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Detalles Bibliográficos
Autores principales: Zhang, G. Q., Yu, S. C. M.
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Hindawi Publishing Corporation 2014
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC3933025/
https://www.ncbi.nlm.nih.gov/pubmed/24683339
http://dx.doi.org/10.1155/2014/410749
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author Zhang, G. Q.
Yu, S. C. M.
author_facet Zhang, G. Q.
Yu, S. C. M.
author_sort Zhang, G. Q.
collection PubMed
description Inspired by superior flight performance of natural flight masters like birds and insects and based on the ventilating flaps that can be opened and closed by the changing air pressure around the wing, a new flapping wing type has been proposed. It is known that the net lift force generated by a solid wing in a flapping cycle is nearly zero. However, for the case of the ventilated wing, results for the net lift force are positive which is due to the effect created by the “ventilation” in reducing negative lift force during the upstroke. The presence of moving flaps can serve as the variable in which, through careful control of the areas, a correlation with the decrease in negative lift can be generated. The corresponding aerodynamic characteristics have been investigated numerically by using different flapping frequencies and forward flight speeds.
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spelling pubmed-39330252014-03-30 Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle Zhang, G. Q. Yu, S. C. M. ScientificWorldJournal Research Article Inspired by superior flight performance of natural flight masters like birds and insects and based on the ventilating flaps that can be opened and closed by the changing air pressure around the wing, a new flapping wing type has been proposed. It is known that the net lift force generated by a solid wing in a flapping cycle is nearly zero. However, for the case of the ventilated wing, results for the net lift force are positive which is due to the effect created by the “ventilation” in reducing negative lift force during the upstroke. The presence of moving flaps can serve as the variable in which, through careful control of the areas, a correlation with the decrease in negative lift can be generated. The corresponding aerodynamic characteristics have been investigated numerically by using different flapping frequencies and forward flight speeds. Hindawi Publishing Corporation 2014-02-06 /pmc/articles/PMC3933025/ /pubmed/24683339 http://dx.doi.org/10.1155/2014/410749 Text en Copyright © 2014 G. Q. Zhang and S. C. M. Yu. https://creativecommons.org/licenses/by/3.0/ This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
spellingShingle Research Article
Zhang, G. Q.
Yu, S. C. M.
Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle
title Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle
title_full Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle
title_fullStr Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle
title_full_unstemmed Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle
title_short Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle
title_sort aerodynamic characteristics of the ventilated design for flapping wing micro air vehicle
topic Research Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC3933025/
https://www.ncbi.nlm.nih.gov/pubmed/24683339
http://dx.doi.org/10.1155/2014/410749
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