Can Scalable Design of Wings for Flapping Wing Micro Air Vehicle Be Inspired by Natural Flyers?

Lift production is constantly a great challenge for flapping wing micro air vehicles (MAVs). Designing a workable wing, therefore, plays an essential role. Dimensional analysis is an effective and valuable tool in studying the biomechanics of flyers. In this paper, geometric similarity study is firs...

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Main Authors: Yanghai Nan, Bei Peng, Yi Chen, Zhenyu Feng, Don McGlinchey
Format: Article
Language:English
Published: Wiley 2018-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2018/9538328
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author Yanghai Nan
Bei Peng
Yi Chen
Zhenyu Feng
Don McGlinchey
author_facet Yanghai Nan
Bei Peng
Yi Chen
Zhenyu Feng
Don McGlinchey
author_sort Yanghai Nan
collection DOAJ
description Lift production is constantly a great challenge for flapping wing micro air vehicles (MAVs). Designing a workable wing, therefore, plays an essential role. Dimensional analysis is an effective and valuable tool in studying the biomechanics of flyers. In this paper, geometric similarity study is firstly presented. Then, the pw−AR ratio is defined and employed in wing performance estimation before the lumped parameter is induced and utilized in wing design. Comprehensive scaling laws on relation of wing performances for natural flyers are next investigated and developed via statistical analysis before being utilized to examine the wing design. Through geometric similarity study and statistical analysis, the results show that the aspect ratio and lumped parameter are independent on mass, and the lumped parameter is inversely proportional to the aspect ratio. The lumped parameters and aspect ratio of flapping wing MAVs correspond to the range of wing performances of natural flyers. Also, the wing performances of existing flapping wing MAVs are examined and follow the scaling laws. Last, the manufactured wings of the flapping wing MAVs are summarized. Our results will, therefore, provide a simple but powerful guideline for biologists and engineers who study the morphology of natural flyers and design flapping wing MAVs.
format Article
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institution Kabale University
issn 1687-5966
1687-5974
language English
publishDate 2018-01-01
publisher Wiley
record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-54f07c19f7ca476abc4b65ab6c90fd942025-02-03T00:59:20ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742018-01-01201810.1155/2018/95383289538328Can Scalable Design of Wings for Flapping Wing Micro Air Vehicle Be Inspired by Natural Flyers?Yanghai Nan0Bei Peng1Yi Chen2Zhenyu Feng3Don McGlinchey4School of Mechanical and Electrical Engineering, University of Electronic Science and Technology of China, Chengdu 611731, ChinaSchool of Mechanical and Electrical Engineering, University of Electronic Science and Technology of China, Chengdu 611731, ChinaSchool of Mechanical and Electrical Engineering, University of Electronic Science and Technology of China, Chengdu 611731, ChinaSchool of Mechanical and Electrical Engineering, University of Electronic Science and Technology of China, Chengdu 611731, ChinaSchool of Engineering and Built Environment, Glasgow Caledonian University, Glasgow G4 0BA, UKLift production is constantly a great challenge for flapping wing micro air vehicles (MAVs). Designing a workable wing, therefore, plays an essential role. Dimensional analysis is an effective and valuable tool in studying the biomechanics of flyers. In this paper, geometric similarity study is firstly presented. Then, the pw−AR ratio is defined and employed in wing performance estimation before the lumped parameter is induced and utilized in wing design. Comprehensive scaling laws on relation of wing performances for natural flyers are next investigated and developed via statistical analysis before being utilized to examine the wing design. Through geometric similarity study and statistical analysis, the results show that the aspect ratio and lumped parameter are independent on mass, and the lumped parameter is inversely proportional to the aspect ratio. The lumped parameters and aspect ratio of flapping wing MAVs correspond to the range of wing performances of natural flyers. Also, the wing performances of existing flapping wing MAVs are examined and follow the scaling laws. Last, the manufactured wings of the flapping wing MAVs are summarized. Our results will, therefore, provide a simple but powerful guideline for biologists and engineers who study the morphology of natural flyers and design flapping wing MAVs.http://dx.doi.org/10.1155/2018/9538328
spellingShingle Yanghai Nan
Bei Peng
Yi Chen
Zhenyu Feng
Don McGlinchey
Can Scalable Design of Wings for Flapping Wing Micro Air Vehicle Be Inspired by Natural Flyers?
International Journal of Aerospace Engineering
title Can Scalable Design of Wings for Flapping Wing Micro Air Vehicle Be Inspired by Natural Flyers?
title_full Can Scalable Design of Wings for Flapping Wing Micro Air Vehicle Be Inspired by Natural Flyers?
title_fullStr Can Scalable Design of Wings for Flapping Wing Micro Air Vehicle Be Inspired by Natural Flyers?
title_full_unstemmed Can Scalable Design of Wings for Flapping Wing Micro Air Vehicle Be Inspired by Natural Flyers?
title_short Can Scalable Design of Wings for Flapping Wing Micro Air Vehicle Be Inspired by Natural Flyers?
title_sort can scalable design of wings for flapping wing micro air vehicle be inspired by natural flyers
url http://dx.doi.org/10.1155/2018/9538328
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AT beipeng canscalabledesignofwingsforflappingwingmicroairvehiclebeinspiredbynaturalflyers
AT yichen canscalabledesignofwingsforflappingwingmicroairvehiclebeinspiredbynaturalflyers
AT zhenyufeng canscalabledesignofwingsforflappingwingmicroairvehiclebeinspiredbynaturalflyers
AT donmcglinchey canscalabledesignofwingsforflappingwingmicroairvehiclebeinspiredbynaturalflyers