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A Computational Fluid Dynamics Investigation of a Novel Ducted Winglet Design / RICHARD DAVIS

Swansea University Author: RICHARD DAVIS

Abstract

Induced drag is a crucial component of the total drag experienced by aircraft,and reducing it can improve their performance. This study investigates theefficacy of a novel ducted wingtip device in reducing induced drag.Computational fluid dynamics simulations were performed on an EmbraerERJ145 aircr...

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Published: Swansea, Wales, UK 2023
Institution: Swansea University
Degree level: Master of Research
Degree name: MSc by Research
Supervisor: Evans, B. J.
URI: https://cronfa.swan.ac.uk/Record/cronfa63503
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first_indexed 2023-05-19T07:57:28Z
last_indexed 2023-05-19T07:57:28Z
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spelling v2 63503 2023-05-19 A Computational Fluid Dynamics Investigation of a Novel Ducted Winglet Design 5f4f5a26cd07c4ea4d5609531e9d8fd6 RICHARD DAVIS RICHARD DAVIS true false 2023-05-19 Induced drag is a crucial component of the total drag experienced by aircraft,and reducing it can improve their performance. This study investigates theefficacy of a novel ducted wingtip device in reducing induced drag.Computational fluid dynamics simulations were performed on an EmbraerERJ145 aircraft with different wingtip configurations, including a ductedwinglet, a conventional winglet, and a standard wingtip, across a range of anglesof attack. Post-processing techniques such as flow visualization and Trefftzplane analysis were employed to examine the performance of the differentwingtip configurations and their induced drag.Results show that the ducted winglet configuration produced lower values of thecoefficient of induced drag across all angles of attack when compared to boththe conventional winglet and standard wingtip. However, it also incurred higherform drag penalties due to eddying and separation behaviour identified at theduct. While the ducted winglet produced similar results for the coefficient oftotal drag at 0 and 1 degree angle of attack compared to both the conventionalwinglet and standard wingtip, it resulted in higher values at 3, 4, and 5 degreesangle of attack.Overall, the study suggests that the design of the ducted winglet can reduceinduced drag and improve aircraft performance. However, further improvementsto the design are necessary to address form drag penalties and enhance itsefficacy. E-Thesis Swansea, Wales, UK Computational Fluid Dynamics, Wingtip Device, Ducted Winglet, Induced Drag, FLITE3D, Spalart-Allmaras, Drag Reduction 4 5 2023 2023-05-04 COLLEGE NANME COLLEGE CODE Swansea University Evans, B. J. Master of Research MSc by Research 2023-10-27T15:34:16.7036100 2023-05-19T08:55:47.5054636 Faculty of Science and Engineering School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering RICHARD DAVIS 1 63503__27530__2681d8d655a649f2aeca8a44df6a2425.pdf 2023_Davis_RJ.final.63503.pdf 2023-05-19T08:58:39.9945621 Output 14254921 application/pdf E-Thesis – open access true Copyright: The Author, Richard J. Davis, 2023. true eng
title A Computational Fluid Dynamics Investigation of a Novel Ducted Winglet Design
spellingShingle A Computational Fluid Dynamics Investigation of a Novel Ducted Winglet Design
RICHARD DAVIS
title_short A Computational Fluid Dynamics Investigation of a Novel Ducted Winglet Design
title_full A Computational Fluid Dynamics Investigation of a Novel Ducted Winglet Design
title_fullStr A Computational Fluid Dynamics Investigation of a Novel Ducted Winglet Design
title_full_unstemmed A Computational Fluid Dynamics Investigation of a Novel Ducted Winglet Design
title_sort A Computational Fluid Dynamics Investigation of a Novel Ducted Winglet Design
author_id_str_mv 5f4f5a26cd07c4ea4d5609531e9d8fd6
author_id_fullname_str_mv 5f4f5a26cd07c4ea4d5609531e9d8fd6_***_RICHARD DAVIS
author RICHARD DAVIS
author2 RICHARD DAVIS
format E-Thesis
publishDate 2023
institution Swansea University
college_str Faculty of Science and Engineering
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title Faculty of Science and Engineering
department_str School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering
document_store_str 1
active_str 0
description Induced drag is a crucial component of the total drag experienced by aircraft,and reducing it can improve their performance. This study investigates theefficacy of a novel ducted wingtip device in reducing induced drag.Computational fluid dynamics simulations were performed on an EmbraerERJ145 aircraft with different wingtip configurations, including a ductedwinglet, a conventional winglet, and a standard wingtip, across a range of anglesof attack. Post-processing techniques such as flow visualization and Trefftzplane analysis were employed to examine the performance of the differentwingtip configurations and their induced drag.Results show that the ducted winglet configuration produced lower values of thecoefficient of induced drag across all angles of attack when compared to boththe conventional winglet and standard wingtip. However, it also incurred higherform drag penalties due to eddying and separation behaviour identified at theduct. While the ducted winglet produced similar results for the coefficient oftotal drag at 0 and 1 degree angle of attack compared to both the conventionalwinglet and standard wingtip, it resulted in higher values at 3, 4, and 5 degreesangle of attack.Overall, the study suggests that the design of the ducted winglet can reduceinduced drag and improve aircraft performance. However, further improvementsto the design are necessary to address form drag penalties and enhance itsefficacy.
published_date 2023-05-04T15:34:14Z
_version_ 1780919571594608640
score 11.016593

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