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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sg-ntu-dr.10356-968842023-03-04T17:17:36Z Aerodynamic characteristics of the ventilated design for flapping wing micro air vehicle Zhang, G. Q. Yu, S. C. M. School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics 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. Published version 2014-06-04T07:10:29Z 2019-12-06T19:36:19Z 2014-06-04T07:10:29Z 2019-12-06T19:36:19Z 2014 2014 Journal Article Zhang, G. Q., & Yu, S. C. M. (2014). Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle. The Scientific World Journal, 2014, 410749-. 1537-744X https://hdl.handle.net/10356/96884 http://hdl.handle.net/10220/19574 10.1155/2014/410749 24683339 en The scientific world journal © 2014 G. Q. Zhang and S. C. M. Yu. 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. application/pdf |
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DRNTU::Engineering::Aeronautical engineering::Aerodynamics Zhang, G. Q. Yu, S. C. M. Aerodynamic characteristics of the ventilated design for flapping wing micro air vehicle |
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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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School of Mechanical and Aerospace Engineering |
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School of Mechanical and Aerospace Engineering Zhang, G. Q. Yu, S. C. M. |
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Article |
author |
Zhang, G. Q. Yu, S. C. M. |
author_sort |
Zhang, G. Q. |
title |
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_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_sort |
aerodynamic characteristics of the ventilated design for flapping wing micro air vehicle |
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2014 |
url |
https://hdl.handle.net/10356/96884 http://hdl.handle.net/10220/19574 |
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1759855319127687168 |