Leading-edge tubercle modifications to the biomimetic wings

An experimental investigation was conducted to better understand the effects of the humpback whale flipper's tubercles on biomimetic models. Different configurations of tubercles were investigated for five biomimetic flipper models by performing force measurement experiments at the Reynolds num...

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Main Authors: colak, Aleyna, Seyhan, Mehmet, Sarioglu, Mustafa
Format: Article in Journal/Newspaper
Language:unknown
Published: 2023
Subjects:
Online Access:https://aperta.ulakbim.gov.tr/record/268940
id ftaperta:oai:aperta.ulakbim.gov.tr:268940
record_format openpolar
spelling ftaperta:oai:aperta.ulakbim.gov.tr:268940 2024-06-23T07:53:36+00:00 Leading-edge tubercle modifications to the biomimetic wings colak, Aleyna Seyhan, Mehmet Sarioglu, Mustafa 2023-01-01 https://aperta.ulakbim.gov.tr/record/268940 unknown https://aperta.ulakbim.gov.tr/record/268940 oai:aperta.ulakbim.gov.tr:268940 info:eu-repo/semantics/openAccess http://www.opendefinition.org/licenses/cc-by PHYSICS OF FLUIDS 35(1) 14 info:eu-repo/semantics/article publication-article 2023 ftaperta 2024-06-12T23:31:53Z An experimental investigation was conducted to better understand the effects of the humpback whale flipper's tubercles on biomimetic models. Different configurations of tubercles were investigated for five biomimetic flipper models by performing force measurement experiments at the Reynolds number of 5.0 x 10(4), 8.0 x 10(4), and 1.2 x 10(5) and surface oil flow visualization at Re = 1.2 x 10(5). The experiments were carried out with five different test models: two baseline models, one having a smooth and one having a tubercle leading-edge (LE); two simply designed tubercle models with uniform distribution; and a proposed tubercle model having a more realistic approach. It is proposed to create a tubercle pattern of a flipper model by summing two wave functions. The results indicated that the models with LE tubercles improved lift, delayed stall angle, and reduced drag compared to the baseline model. Irrespective of the Reynolds number, the model C3, which was created with a more realistic approach, performs better compared to baseline and other tubercle models. It has been seen that the maximum improvement in lift coefficient is achieved by approximately 18% with the C3 model at Re = 5.0 x 10(4). According to flow visualization results, the laminar separation bubble formed in the smooth baseline model was replaced by a counter-rotating vortex pairs (CRVPs) in the tubercle models. The improvement of the aerodynamic characteristics is due to the CRVPs formed by the interaction of the LE tubercles with each other and wavelike trailing-edge flow separation pattern. One of the significant findings to emerge from this study is that a more realistic approach has the potential to obtain better performance than a model with a uniform distribution of tubercles. Article in Journal/Newspaper Humpback Whale Aperta - Türkiye Açık Arşiv
institution Open Polar
collection Aperta - Türkiye Açık Arşiv
op_collection_id ftaperta
language unknown
description An experimental investigation was conducted to better understand the effects of the humpback whale flipper's tubercles on biomimetic models. Different configurations of tubercles were investigated for five biomimetic flipper models by performing force measurement experiments at the Reynolds number of 5.0 x 10(4), 8.0 x 10(4), and 1.2 x 10(5) and surface oil flow visualization at Re = 1.2 x 10(5). The experiments were carried out with five different test models: two baseline models, one having a smooth and one having a tubercle leading-edge (LE); two simply designed tubercle models with uniform distribution; and a proposed tubercle model having a more realistic approach. It is proposed to create a tubercle pattern of a flipper model by summing two wave functions. The results indicated that the models with LE tubercles improved lift, delayed stall angle, and reduced drag compared to the baseline model. Irrespective of the Reynolds number, the model C3, which was created with a more realistic approach, performs better compared to baseline and other tubercle models. It has been seen that the maximum improvement in lift coefficient is achieved by approximately 18% with the C3 model at Re = 5.0 x 10(4). According to flow visualization results, the laminar separation bubble formed in the smooth baseline model was replaced by a counter-rotating vortex pairs (CRVPs) in the tubercle models. The improvement of the aerodynamic characteristics is due to the CRVPs formed by the interaction of the LE tubercles with each other and wavelike trailing-edge flow separation pattern. One of the significant findings to emerge from this study is that a more realistic approach has the potential to obtain better performance than a model with a uniform distribution of tubercles.
format Article in Journal/Newspaper
author colak, Aleyna
Seyhan, Mehmet
Sarioglu, Mustafa
spellingShingle colak, Aleyna
Seyhan, Mehmet
Sarioglu, Mustafa
Leading-edge tubercle modifications to the biomimetic wings
author_facet colak, Aleyna
Seyhan, Mehmet
Sarioglu, Mustafa
author_sort colak, Aleyna
title Leading-edge tubercle modifications to the biomimetic wings
title_short Leading-edge tubercle modifications to the biomimetic wings
title_full Leading-edge tubercle modifications to the biomimetic wings
title_fullStr Leading-edge tubercle modifications to the biomimetic wings
title_full_unstemmed Leading-edge tubercle modifications to the biomimetic wings
title_sort leading-edge tubercle modifications to the biomimetic wings
publishDate 2023
url https://aperta.ulakbim.gov.tr/record/268940
genre Humpback Whale
genre_facet Humpback Whale
op_source PHYSICS OF FLUIDS 35(1) 14
op_relation https://aperta.ulakbim.gov.tr/record/268940
oai:aperta.ulakbim.gov.tr:268940
op_rights info:eu-repo/semantics/openAccess
http://www.opendefinition.org/licenses/cc-by
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