Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control
The Leading Edge Cylinder Aerofoil has resulted in an outpour of research studies for almost a century till date but fewer attempt has focused on the embedment of a cylinder with undercambered aerofoil. This research was aimed to ascertain whether the concept could enhance the intended aerofoil’s ae...
| Main Authors: | , , |
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| Format: | Article |
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Aeronautical and Astronautical Society of the Republic of China
2021
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| Online Access: | http://psasir.upm.edu.my/id/eprint/94388/ |
| _version_ | 1848861983611289600 |
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| author | Mohammad Ali, Hidayatullah Mohd Rafie, Azmin Shakrine Md Ali, Syaril Azrad |
| author_facet | Mohammad Ali, Hidayatullah Mohd Rafie, Azmin Shakrine Md Ali, Syaril Azrad |
| author_sort | Mohammad Ali, Hidayatullah |
| building | UPM Institutional Repository |
| collection | Online Access |
| description | The Leading Edge Cylinder Aerofoil has resulted in an outpour of research studies for almost a century till date but fewer attempt has focused on the embedment of a cylinder with undercambered aerofoil. This research was aimed to ascertain whether the concept could enhance the intended aerofoil’s aerodynamic properties. The performance of the model was tested using computational fluid dynamic code ANSYS Workbench 2019 to simulate two-dimensional flow analysis with a variant of rotational speed up to 2000 RPM for different free stream speeds ranging from 5 to 30 m/s at various angles of attacks with the Reynolds number ranged from 4.56E+05 to 2.74E+06. The mesh independency test has been validated with an error of less than 1% prior to designing the best model embedment. The analysis resulted in an enhancement in the lift coefficient and stall angle delay of about 23% and 61%, respectively. |
| first_indexed | 2025-11-15T13:09:48Z |
| format | Article |
| id | upm-94388 |
| institution | Universiti Putra Malaysia |
| institution_category | Local University |
| last_indexed | 2025-11-15T13:09:48Z |
| publishDate | 2021 |
| publisher | Aeronautical and Astronautical Society of the Republic of China |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | upm-943882023-04-05T01:44:30Z http://psasir.upm.edu.my/id/eprint/94388/ Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control Mohammad Ali, Hidayatullah Mohd Rafie, Azmin Shakrine Md Ali, Syaril Azrad The Leading Edge Cylinder Aerofoil has resulted in an outpour of research studies for almost a century till date but fewer attempt has focused on the embedment of a cylinder with undercambered aerofoil. This research was aimed to ascertain whether the concept could enhance the intended aerofoil’s aerodynamic properties. The performance of the model was tested using computational fluid dynamic code ANSYS Workbench 2019 to simulate two-dimensional flow analysis with a variant of rotational speed up to 2000 RPM for different free stream speeds ranging from 5 to 30 m/s at various angles of attacks with the Reynolds number ranged from 4.56E+05 to 2.74E+06. The mesh independency test has been validated with an error of less than 1% prior to designing the best model embedment. The analysis resulted in an enhancement in the lift coefficient and stall angle delay of about 23% and 61%, respectively. Aeronautical and Astronautical Society of the Republic of China 2021-01 Article PeerReviewed Mohammad Ali, Hidayatullah and Mohd Rafie, Azmin Shakrine and Md Ali, Syaril Azrad (2021) Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control. Journal of Aeronautics, Astronautics and Aviation, 53 (2). 143 - 153. ISSN 1990-7710 https://www.airitilibrary.com/Publication/alDetailedMesh?DocID=P20140627004-202106-202102080001-202102080001-143-153 10.6125/JoAAA.202106_53(2).06 |
| spellingShingle | Mohammad Ali, Hidayatullah Mohd Rafie, Azmin Shakrine Md Ali, Syaril Azrad Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control |
| title | Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control |
| title_full | Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control |
| title_fullStr | Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control |
| title_full_unstemmed | Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control |
| title_short | Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control |
| title_sort | numerical analysis of leading edge cylinder aerofoil on selig s1223 for moving surface boundary control |
| url | http://psasir.upm.edu.my/id/eprint/94388/ http://psasir.upm.edu.my/id/eprint/94388/ http://psasir.upm.edu.my/id/eprint/94388/ |