The leading-edge vortex of swift wing-shaped delta wings

Recent investigations on the aerodynamics of natural fliers have illuminated the significance of the leading-edge vortex (LEV) for lift generation in a variety of flight conditions. A well-documented example of an LEV is that generated by aircraft with highly swept, delta-shaped wings. While the win...

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Published in:Royal Society Open Science
Main Authors: Muir, Rowan Eveline, Arredondo-Galeana, Abel, Viola, Ignazio Maria
Other Authors: Consejo Nacional de Ciencia y Tecnología, Engineering and Physical Sciences Research Council
Format: Article in Journal/Newspaper
Language:English
Published: The Royal Society 2017
Subjects:
Online Access:http://dx.doi.org/10.1098/rsos.170077
https://royalsocietypublishing.org/doi/pdf/10.1098/rsos.170077
https://royalsocietypublishing.org/doi/full-xml/10.1098/rsos.170077
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spelling crroyalsociety:10.1098/rsos.170077 2024-09-15T17:49:29+00:00 The leading-edge vortex of swift wing-shaped delta wings Muir, Rowan Eveline Arredondo-Galeana, Abel Viola, Ignazio Maria Consejo Nacional de Ciencia y Tecnología Engineering and Physical Sciences Research Council 2017 http://dx.doi.org/10.1098/rsos.170077 https://royalsocietypublishing.org/doi/pdf/10.1098/rsos.170077 https://royalsocietypublishing.org/doi/full-xml/10.1098/rsos.170077 en eng The Royal Society https://royalsociety.org/journals/ethics-policies/data-sharing-mining/ Royal Society Open Science volume 4, issue 8, page 170077 ISSN 2054-5703 journal-article 2017 crroyalsociety https://doi.org/10.1098/rsos.170077 2024-08-12T04:27:50Z Recent investigations on the aerodynamics of natural fliers have illuminated the significance of the leading-edge vortex (LEV) for lift generation in a variety of flight conditions. A well-documented example of an LEV is that generated by aircraft with highly swept, delta-shaped wings. While the wing aerodynamics of a manoeuvring aircraft, a bird gliding and a bird in flapping flight vary significantly, it is believed that this existing knowledge can serve to add understanding to the complex aerodynamics of natural fliers. In this investigation, a model non-slender delta-shaped wing with a sharp leading edge is tested at low Reynolds number, along with a delta wing of the same design, but with a modified trailing edge inspired by the wing of a common swift Apus apus . The effect of the tapering swift wing on LEV development and stability is compared with the flow structure over the unmodified delta wing model through particle image velocimetry. For the first time, a leading-edge vortex system consisting of a dual or triple LEV is recorded on a swift wing-shaped delta wing, where such a system is found across all tested conditions. It is shown that the spanwise location of LEV breakdown is governed by the local chord rather than Reynolds number or angle of attack. These findings suggest that the trailing-edge geometry of the swift wing alone does not prevent the common swift from generating an LEV system comparable with that of a delta-shaped wing. Article in Journal/Newspaper Apus apus The Royal Society Royal Society Open Science 4 8 170077
institution Open Polar
collection The Royal Society
op_collection_id crroyalsociety
language English
description Recent investigations on the aerodynamics of natural fliers have illuminated the significance of the leading-edge vortex (LEV) for lift generation in a variety of flight conditions. A well-documented example of an LEV is that generated by aircraft with highly swept, delta-shaped wings. While the wing aerodynamics of a manoeuvring aircraft, a bird gliding and a bird in flapping flight vary significantly, it is believed that this existing knowledge can serve to add understanding to the complex aerodynamics of natural fliers. In this investigation, a model non-slender delta-shaped wing with a sharp leading edge is tested at low Reynolds number, along with a delta wing of the same design, but with a modified trailing edge inspired by the wing of a common swift Apus apus . The effect of the tapering swift wing on LEV development and stability is compared with the flow structure over the unmodified delta wing model through particle image velocimetry. For the first time, a leading-edge vortex system consisting of a dual or triple LEV is recorded on a swift wing-shaped delta wing, where such a system is found across all tested conditions. It is shown that the spanwise location of LEV breakdown is governed by the local chord rather than Reynolds number or angle of attack. These findings suggest that the trailing-edge geometry of the swift wing alone does not prevent the common swift from generating an LEV system comparable with that of a delta-shaped wing.
author2 Consejo Nacional de Ciencia y Tecnología
Engineering and Physical Sciences Research Council
format Article in Journal/Newspaper
author Muir, Rowan Eveline
Arredondo-Galeana, Abel
Viola, Ignazio Maria
spellingShingle Muir, Rowan Eveline
Arredondo-Galeana, Abel
Viola, Ignazio Maria
The leading-edge vortex of swift wing-shaped delta wings
author_facet Muir, Rowan Eveline
Arredondo-Galeana, Abel
Viola, Ignazio Maria
author_sort Muir, Rowan Eveline
title The leading-edge vortex of swift wing-shaped delta wings
title_short The leading-edge vortex of swift wing-shaped delta wings
title_full The leading-edge vortex of swift wing-shaped delta wings
title_fullStr The leading-edge vortex of swift wing-shaped delta wings
title_full_unstemmed The leading-edge vortex of swift wing-shaped delta wings
title_sort leading-edge vortex of swift wing-shaped delta wings
publisher The Royal Society
publishDate 2017
url http://dx.doi.org/10.1098/rsos.170077
https://royalsocietypublishing.org/doi/pdf/10.1098/rsos.170077
https://royalsocietypublishing.org/doi/full-xml/10.1098/rsos.170077
genre Apus apus
genre_facet Apus apus
op_source Royal Society Open Science
volume 4, issue 8, page 170077
ISSN 2054-5703
op_rights https://royalsociety.org/journals/ethics-policies/data-sharing-mining/
op_doi https://doi.org/10.1098/rsos.170077
container_title Royal Society Open Science
container_volume 4
container_issue 8
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