Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number
This study is to investigate the aerodynamic characteristic of an airfoil in low Reynolds number flow. NACA2415 airfoil is chosen as the test subject as it has been studied by many researches and documented. Coordinate point of NACA2415 is generated by using NACA 4 Digits Series Profile Generator, a...
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| Format: | Undergraduates Project Papers |
| Language: | English English English |
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2013
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| Online Access: | http://umpir.ump.edu.my/id/eprint/7623/ http://umpir.ump.edu.my/id/eprint/7623/ http://umpir.ump.edu.my/id/eprint/7623/1/CD7737.pdf http://umpir.ump.edu.my/id/eprint/7623/4/1.pdf http://umpir.ump.edu.my/id/eprint/7623/10/3.pdf |
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ump-7623 |
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eprints |
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ump-76232015-11-20T12:31:21Z http://umpir.ump.edu.my/id/eprint/7623/ Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number Muhammad Hafizuddin , Ismail TK Electrical engineering. Electronics Nuclear engineering This study is to investigate the aerodynamic characteristic of an airfoil in low Reynolds number flow. NACA2415 airfoil is chosen as the test subject as it has been studied by many researches and documented. Coordinate point of NACA2415 is generated by using NACA 4 Digits Series Profile Generator, a web-based Java applet before being used by ANSYS Fluent to create 2D geometry of the airfoil. In the simulation, the boundary condition is set mimicking the streamline flowing at an angle ranging from 0 degree to 20 degree. As for the velocity, it is set for a flow condition under the Reynolds number of 200000 in incompressible viscous medium. From the simulation data, the Cd, Cl, Cp and the formation of Laminar Separation Bubble becoming the main concern for the simulation. Validation test is performed to approve the validity of the simulation result. Unfortunately, this investigation comes to a hold since the validation test is failed to capture the formation of LSB. The factor leading to the error is discussed. 2013-06 Undergraduates Project Papers NonPeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/7623/1/CD7737.pdf application/pdf en http://umpir.ump.edu.my/id/eprint/7623/4/1.pdf application/pdf en http://umpir.ump.edu.my/id/eprint/7623/10/3.pdf Muhammad Hafizuddin , Ismail (2013) Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number. Faculty of Manufacturing Engineering, Universiti Malaysia Pahang. http://iportal.ump.edu.my/lib/item?id=chamo:78519&theme=UMP2 |
| repository_type |
Digital Repository |
| institution_category |
Local University |
| institution |
Universiti Malaysia Pahang |
| building |
UMP Institutional Repository |
| collection |
Online Access |
| language |
English English English |
| topic |
TK Electrical engineering. Electronics Nuclear engineering |
| spellingShingle |
TK Electrical engineering. Electronics Nuclear engineering Muhammad Hafizuddin , Ismail Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number |
| description |
This study is to investigate the aerodynamic characteristic of an airfoil in low Reynolds number flow. NACA2415 airfoil is chosen as the test subject as it has been studied by many researches and documented. Coordinate point of NACA2415 is generated by using NACA 4 Digits Series Profile Generator, a web-based Java applet before being used by ANSYS Fluent to create 2D geometry of the airfoil. In the simulation, the boundary condition is set mimicking the streamline flowing at an angle ranging from 0 degree to 20 degree. As for the velocity, it is set for a flow condition under the Reynolds number of 200000 in incompressible viscous medium. From the simulation data, the Cd, Cl, Cp and the formation of Laminar Separation Bubble becoming the main concern for the simulation. Validation test is performed to approve the validity of the simulation result. Unfortunately, this investigation comes to a hold since the validation test is failed to capture the formation of LSB. The factor leading to the error is discussed. |
| format |
Undergraduates Project Papers |
| author |
Muhammad Hafizuddin , Ismail |
| author_facet |
Muhammad Hafizuddin , Ismail |
| author_sort |
Muhammad Hafizuddin , Ismail |
| title |
Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number |
| title_short |
Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number |
| title_full |
Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number |
| title_fullStr |
Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number |
| title_full_unstemmed |
Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number |
| title_sort |
parametric investigation on the aerodynamic characteristic of naca2415 airfoil at low reynolds number |
| publishDate |
2013 |
| url |
http://umpir.ump.edu.my/id/eprint/7623/ http://umpir.ump.edu.my/id/eprint/7623/ http://umpir.ump.edu.my/id/eprint/7623/1/CD7737.pdf http://umpir.ump.edu.my/id/eprint/7623/4/1.pdf http://umpir.ump.edu.my/id/eprint/7623/10/3.pdf |
| first_indexed |
2023-09-18T22:04:25Z |
| last_indexed |
2023-09-18T22:04:25Z |
| _version_ |
1777414612190232576 |