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...
Saved in:
| Main Author: | |
|---|---|
| Format: | Thesis |
| Language: | en |
| Published: |
2023
|
| Subjects: | |
| Online Access: | https://ir.uitm.edu.my/id/eprint/106984/1/106984.pdf https://ir.uitm.edu.my/id/eprint/106984/ |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1833323265222770688 |
|---|---|
| author | Ramli, Muhammad Ridzwan |
| author_facet | Ramli, Muhammad Ridzwan |
| author_sort | Ramli, Muhammad Ridzwan |
| building | Tun Abdul Razak Library |
| collection | Institutional Repository |
| content_provider | Universiti Teknologi Mara |
| content_source | UiTM Institutional Repository |
| continent | Asia |
| country | Malaysia |
| 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 |
| id | my.uitm.ir-106984 |
| institution | Universiti Teknologi Mara |
| language | en |
| publishDate | 2023 |
| record_format | eprints |
| spelling | my.uitm.ir-1069842025-04-18T06:09:56Z https://ir.uitm.edu.my/id/eprint/106984/ Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli 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 NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/106984/1/106984.pdf Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli. (2023) Masters thesis, thesis, Universiti Teknologi MARA (UiTM). <http://terminalib.uitm.edu.my/106984.pdf> |
| spellingShingle | Engineering mathematics. Engineering analysis Ramli, Muhammad Ridzwan Simulation of multi tip-sail winglet for drag reduction at mach 0.1 / Muhammad Ridzwan Ramli |
| title | 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_short | 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 |
| topic | Engineering mathematics. Engineering analysis |
| url | https://ir.uitm.edu.my/id/eprint/106984/1/106984.pdf https://ir.uitm.edu.my/id/eprint/106984/ |
| url_provider | http://ir.uitm.edu.my/ |