Effects of airfoil on aerodynamic performance of flapping wing Article Swipe
Min Zhao
,
Yao Zou
,
Qiang Fu
,
Wei He
·
YOU?
·
· 2021
· Open Access
·
· DOI: https://doi.org/10.1016/j.birob.2021.100004
YOU?
·
· 2021
· Open Access
·
· DOI: https://doi.org/10.1016/j.birob.2021.100004
Flapping-wing aircraft (FWA) operates in a flight mode that mimics natural flyers, such as birds, bats and insects. For large scale bird-inspired flapping wings aircraft, the design of airfoil parameters is crucial to improving the aerodynamic performance. In order to study the effect of camber on the aerodynamic characteristics, we developed four different airfoils with a chord length of 12 cm. The cambers of airfoils are respectively 30 mm, 25 mm, 20 mm and 15 mm. A numerical investigation into the effects of camber on aerodynamic performance is carried out through COMSOL Multiphysics software using Fluid–Structure Interaction (FSI) module. In this work, the fluid–structure module employs the Navier–Stokes equations coupled with a solid stress–strain physics module and a moving mesh module. The three-dimensional (3D) flapping wing computational models with different cambers are built. The results show that certain camber of airfoil can improve the aerodynamic characteristics of flapping wing.
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Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.1016/j.birob.2021.100004
- OA Status
- gold
- Cited By
- 8
- References
- 27
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W3163942386
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W3163942386Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.1016/j.birob.2021.100004Digital Object Identifier
- Title
-
Effects of airfoil on aerodynamic performance of flapping wingWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2021Year of publication
- Publication date
-
2021-05-11Full publication date if available
- Authors
-
Min Zhao, Yao Zou, Qiang Fu, Wei HeList of authors in order
- Landing page
-
https://doi.org/10.1016/j.birob.2021.100004Publisher landing page
- Open access
-
YesWhether a free full text is available
- OA status
-
goldOpen access status per OpenAlex
- OA URL
-
https://doi.org/10.1016/j.birob.2021.100004Direct OA link when available
- Concepts
-
Airfoil, Camber (aerodynamics), Flapping, Aerodynamics, Wing, Wing twist, Aerospace engineering, Structural engineering, Chord (peer-to-peer), Multiphysics, Aerodynamic force, Angle of attack, Engineering, Computer science, Finite element method, Distributed computingTop concepts (fields/topics) attached by OpenAlex
- Cited by
-
8Total citation count in OpenAlex
- Citations by year (recent)
-
2025: 3, 2024: 1, 2023: 4Per-year citation counts (last 5 years)
- References (count)
-
27Number of works referenced by this work
- Related works (count)
-
10Other works algorithmically related by OpenAlex
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| primary_location.landing_page_url | https://doi.org/10.1016/j.birob.2021.100004 |
| publication_date | 2021-05-11 |
| publication_year | 2021 |
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