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Aerodynamics and three-dimensional effect of a translating bristled wing at low Reynolds numbers
The smallest insects fly with bristled wings at very low Reynolds numbers (Re) and use the drag of the wings to provide the weight-supporting force and thrust. Previous studies used two-dimensional (2-D) models to study the aerodynamic force and the detailed flow field of the bristled wings, neglect...
Autores principales: | , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Nature Publishing Group UK
2022
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9440148/ https://www.ncbi.nlm.nih.gov/pubmed/36056054 http://dx.doi.org/10.1038/s41598-022-18834-0 |
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author | Liu, Wenjie Sun, Mao |
author_facet | Liu, Wenjie Sun, Mao |
author_sort | Liu, Wenjie |
collection | PubMed |
description | The smallest insects fly with bristled wings at very low Reynolds numbers (Re) and use the drag of the wings to provide the weight-supporting force and thrust. Previous studies used two-dimensional (2-D) models to study the aerodynamic force and the detailed flow field of the bristled wings, neglecting the three-dimensional (3-D) effect caused by the finite span. At high Re, the 3-D effect is known to decrease the aerodynamic force on a body, compared with the 2-D case. However, the bristled wing operates at very low Re, for which the 3-D effect is unknown. Here, a 3-D model of the bristled wing is constructed to numerically investigate the detailed flow field and the aerodynamic force of the wing. Our findings are as follows: The 3-D effect at low Re increases the drag of the bristled wing compared with that of the corresponding 2-D wing, which is contrary to that of the high-Re case. The drag increase is limited to the tip region of the bristles and could be explained by the increase of the flow velocity around the tip region. The spanwise length of the drag-increasing region (measuring from the wing tip) is about 0.23 chord length and does not vary as the wing aspect ratio increases. The amount of the drag increment in the tip region does not vary as the wing aspect ratio increases either, leading to the decrease of the drag coefficient with increasing aspect ratio. |
format | Online Article Text |
id | pubmed-9440148 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2022 |
publisher | Nature Publishing Group UK |
record_format | MEDLINE/PubMed |
spelling | pubmed-94401482022-09-04 Aerodynamics and three-dimensional effect of a translating bristled wing at low Reynolds numbers Liu, Wenjie Sun, Mao Sci Rep Article The smallest insects fly with bristled wings at very low Reynolds numbers (Re) and use the drag of the wings to provide the weight-supporting force and thrust. Previous studies used two-dimensional (2-D) models to study the aerodynamic force and the detailed flow field of the bristled wings, neglecting the three-dimensional (3-D) effect caused by the finite span. At high Re, the 3-D effect is known to decrease the aerodynamic force on a body, compared with the 2-D case. However, the bristled wing operates at very low Re, for which the 3-D effect is unknown. Here, a 3-D model of the bristled wing is constructed to numerically investigate the detailed flow field and the aerodynamic force of the wing. Our findings are as follows: The 3-D effect at low Re increases the drag of the bristled wing compared with that of the corresponding 2-D wing, which is contrary to that of the high-Re case. The drag increase is limited to the tip region of the bristles and could be explained by the increase of the flow velocity around the tip region. The spanwise length of the drag-increasing region (measuring from the wing tip) is about 0.23 chord length and does not vary as the wing aspect ratio increases. The amount of the drag increment in the tip region does not vary as the wing aspect ratio increases either, leading to the decrease of the drag coefficient with increasing aspect ratio. Nature Publishing Group UK 2022-09-02 /pmc/articles/PMC9440148/ /pubmed/36056054 http://dx.doi.org/10.1038/s41598-022-18834-0 Text en © The Author(s) 2022 https://creativecommons.org/licenses/by/4.0/Open AccessThis article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made. The images or other third party material in this article are included in the article's Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article's Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/ (https://creativecommons.org/licenses/by/4.0/) . |
spellingShingle | Article Liu, Wenjie Sun, Mao Aerodynamics and three-dimensional effect of a translating bristled wing at low Reynolds numbers |
title | Aerodynamics and three-dimensional effect of a translating bristled wing at low Reynolds numbers |
title_full | Aerodynamics and three-dimensional effect of a translating bristled wing at low Reynolds numbers |
title_fullStr | Aerodynamics and three-dimensional effect of a translating bristled wing at low Reynolds numbers |
title_full_unstemmed | Aerodynamics and three-dimensional effect of a translating bristled wing at low Reynolds numbers |
title_short | Aerodynamics and three-dimensional effect of a translating bristled wing at low Reynolds numbers |
title_sort | aerodynamics and three-dimensional effect of a translating bristled wing at low reynolds numbers |
topic | Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9440148/ https://www.ncbi.nlm.nih.gov/pubmed/36056054 http://dx.doi.org/10.1038/s41598-022-18834-0 |
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