Ramli, Muhammad Ridzwan
(2023)
Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli.
Masters thesis, Universiti Teknologi MARA (UiTM).
Abstract
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.
Metadata
Item Type: | Thesis (Masters) |
---|---|
Creators: | Creators Email / ID Num. Ramli, Muhammad Ridzwan UNSPECIFIED |
Contributors: | Contribution Name Email / ID Num. Thesis advisor Wan Mohamed, Wan Mazlina UNSPECIFIED |
Subjects: | T Technology > TA Engineering. Civil engineering > Engineering mathematics. Engineering analysis |
Divisions: | Universiti Teknologi MARA, Shah Alam > Malaysia Institute of Transport (MITRANS) |
Programme: | Master of Science |
Keywords: | Aerodynamic characteristics, winglet structures |
Date: | 2023 |
URI: | https://ir.uitm.edu.my/id/eprint/106984 |
Download
Text
106984.pdf
Download (270kB)
106984.pdf
Download (270kB)
Digital Copy
Digital (fulltext) is available at:
Physical Copy
Physical status and holdings:
Item Status: