The effects of vortex shedding on the aerodynamic performance of airfoils
This is a comparative study involving various National Advisory Committee for Aeronautics (NACA) airfoils NACA 0012, NACA 0024, NACA 4412 and NACA 4424. The numerical simulation involves the air flow passing these models at high Reynolds number and various angles of attack. The study focuses mainly...
Saved in:
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | en |
| Published: |
Asian Research Publishing Network (ARPN)
2018
|
| Subjects: | |
| Online Access: | http://eprints.uthm.edu.my/6031/1/AJ%202018%20%28981%29%20The%20effects%20of%20vortex%20shedding%20on%20the%20aerodynamic%20performance%20of%20airfoils%20%20.pdf http://eprints.uthm.edu.my/6031/ |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1833417990676152320 |
|---|---|
| author | Sikien, Esther Rami Abdullah, Aslam Zulkafli, Mohd Fadhli Rahim, Mohammad Zulafif |
| author_facet | Sikien, Esther Rami Abdullah, Aslam Zulkafli, Mohd Fadhli Rahim, Mohammad Zulafif |
| author_sort | Sikien, Esther Rami |
| building | UTHM Library |
| collection | Institutional Repository |
| content_provider | Universiti Tun Hussein Onn Malaysia |
| content_source | UTHM Institutional Repository |
| continent | Asia |
| country | Malaysia |
| description | This is a comparative study involving various National Advisory Committee for Aeronautics (NACA) airfoils NACA 0012, NACA 0024, NACA 4412 and NACA 4424. The numerical simulation involves the air flow passing these models at high Reynolds number and various angles of attack. The study focuses mainly on the aerodynamic performance as represented by lift and drag coefficients. The Computational Fluid Dynamics simulation has been carried out in order to understand the phenomena of vortex shedding. The aim is to investigate the effects of vortex shedding on the aerodynamic performance of airfoils which has still been widely discussed over the years. The methodology has been validated; by using Spalart-Allmaras, K-epsilon and inviscid models, the first with the turbulence intensity and backflow of 0.10% contributed to relatively accurate result. The outcome reveals that there are few aspects that need to be considered in order to control or delay vortex shedding phenomena such as thickness-to-chord ratio, airfoil types, Reynolds number and whether or not it involves transient flow. |
| format | Article |
| id | my.uthm.eprints-6031 |
| institution | Universiti Tun Hussein Onn Malaysia |
| language | en |
| publishDate | 2018 |
| publisher | Asian Research Publishing Network (ARPN) |
| record_format | eprints |
| spelling | my.uthm.eprints-60312022-01-26T02:41:55Z http://eprints.uthm.edu.my/6031/ The effects of vortex shedding on the aerodynamic performance of airfoils Sikien, Esther Rami Abdullah, Aslam Zulkafli, Mohd Fadhli Rahim, Mohammad Zulafif TL500-777 Aeronautics. Aeronautical engineering This is a comparative study involving various National Advisory Committee for Aeronautics (NACA) airfoils NACA 0012, NACA 0024, NACA 4412 and NACA 4424. The numerical simulation involves the air flow passing these models at high Reynolds number and various angles of attack. The study focuses mainly on the aerodynamic performance as represented by lift and drag coefficients. The Computational Fluid Dynamics simulation has been carried out in order to understand the phenomena of vortex shedding. The aim is to investigate the effects of vortex shedding on the aerodynamic performance of airfoils which has still been widely discussed over the years. The methodology has been validated; by using Spalart-Allmaras, K-epsilon and inviscid models, the first with the turbulence intensity and backflow of 0.10% contributed to relatively accurate result. The outcome reveals that there are few aspects that need to be considered in order to control or delay vortex shedding phenomena such as thickness-to-chord ratio, airfoil types, Reynolds number and whether or not it involves transient flow. Asian Research Publishing Network (ARPN) 2018 Article PeerReviewed text en http://eprints.uthm.edu.my/6031/1/AJ%202018%20%28981%29%20The%20effects%20of%20vortex%20shedding%20on%20the%20aerodynamic%20performance%20of%20airfoils%20%20.pdf Sikien, Esther Rami and Abdullah, Aslam and Zulkafli, Mohd Fadhli and Rahim, Mohammad Zulafif (2018) The effects of vortex shedding on the aerodynamic performance of airfoils. ARPN Journal of Engineering and Applied Sciences, 13 (24). pp. 9344-9351. ISSN 1819-6608 |
| spellingShingle | TL500-777 Aeronautics. Aeronautical engineering Sikien, Esther Rami Abdullah, Aslam Zulkafli, Mohd Fadhli Rahim, Mohammad Zulafif The effects of vortex shedding on the aerodynamic performance of airfoils |
| title | The effects of vortex shedding on the aerodynamic performance of airfoils |
| title_full | The effects of vortex shedding on the aerodynamic performance of airfoils |
| title_fullStr | The effects of vortex shedding on the aerodynamic performance of airfoils |
| title_full_unstemmed | The effects of vortex shedding on the aerodynamic performance of airfoils |
| title_short | The effects of vortex shedding on the aerodynamic performance of airfoils |
| title_sort | effects of vortex shedding on the aerodynamic performance of airfoils |
| topic | TL500-777 Aeronautics. Aeronautical engineering |
| url | http://eprints.uthm.edu.my/6031/1/AJ%202018%20%28981%29%20The%20effects%20of%20vortex%20shedding%20on%20the%20aerodynamic%20performance%20of%20airfoils%20%20.pdf http://eprints.uthm.edu.my/6031/ |
| url_provider | http://eprints.uthm.edu.my/ |