Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli

Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli

The flying mechanism is unable to escape from the drag force, especially the drag force generated from the wingtip and trailing edge vortices due to the unbalanced pressure between the upper and lower surface. Then, Richard T. Whitcomb, the scientist at NASA Laboratory introduced the winglet structu...

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Main Author: Ramli, Muhammad Ridzwan
Format: Thesis
Language:English
Published: 2023
Subjects:
Engineering mathematics
Engineering analysis
Online Access:https://ir.uitm.edu.my/id/eprint/106984/1/106984.pdf
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spelling my-uitm-ir.1069842024-11-29T09:19:29Z Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli 2023 Ramli, Muhammad Ridzwan Engineering mathematics. Engineering analysis The flying mechanism is unable to escape from the drag force, especially the drag force generated from the wingtip and trailing edge vortices due to the unbalanced pressure between the upper and lower surface. Then, Richard T. Whitcomb, the scientist at NASA Laboratory introduced the winglet structure, which is functional to reduce the wingtip and trailing edge vortices from the wing structure. However, the current winglet structure that has been installed to the flying mechanism still has room for improvement referred to the mother of nature. Birds usually display their characteristics on hovering and soaring longer in the air by extending their primary feathers. 2023 Thesis https://ir.uitm.edu.my/id/eprint/106984/ https://ir.uitm.edu.my/id/eprint/106984/1/106984.pdf text en public masters Universiti Teknologi MARA (UiTM) Malaysia Institute of Transport (MITRANS) Wan Mohamed, Wan Mazlina
institution Universiti Teknologi MARA
collection UiTM Institutional Repository
language English
advisor Wan Mohamed, Wan Mazlina
topic Engineering mathematics
Engineering analysis
spellingShingle Engineering mathematics
Engineering analysis
Ramli, Muhammad Ridzwan
Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli
description The flying mechanism is unable to escape from the drag force, especially the drag force generated from the wingtip and trailing edge vortices due to the unbalanced pressure between the upper and lower surface. Then, Richard T. Whitcomb, the scientist at NASA Laboratory introduced the winglet structure, which is functional to reduce the wingtip and trailing edge vortices from the wing structure. However, the current winglet structure that has been installed to the flying mechanism still has room for improvement referred to the mother of nature. Birds usually display their characteristics on hovering and soaring longer in the air by extending their primary feathers.
format Thesis
qualification_level Master's degree
author Ramli, Muhammad Ridzwan
author_facet Ramli, Muhammad Ridzwan
author_sort Ramli, Muhammad Ridzwan
title Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli
title_short Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli
title_full Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli
title_fullStr Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli
title_full_unstemmed Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli
title_sort simulation of multi tip-sail winglet for drag reduction at mach 0.1 / muhammad ridzwan ramli
granting_institution Universiti Teknologi MARA (UiTM)
granting_department Malaysia Institute of Transport (MITRANS)
publishDate 2023
url https://ir.uitm.edu.my/id/eprint/106984/1/106984.pdf
_version_ 1818588198813564928

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