Muhammad Hafizuddin, Ismail (2013) Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number. Faculty of Manufacturing Engineering, Universiti Malaysia Pahang.
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Abstract
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.
| Item Type: | Undergraduates Project Papers |
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| Additional Information: | Project paper (Bachor of Mechatronics Engineering) -- Universiti Malaysia Pahang -- 2013, SV: MR. SHAIFUL HAKIM BIN MOHAMED NOOR, CD NO.: 7737 |
| Uncontrolled Keywords: | Aerodynamic airfoil |
| Subjects: | T Technology > TK Electrical engineering. Electronics Nuclear engineering |
| Faculty/Division: | Faculty of Manufacturing Engineering |
| Depositing User: | nurudin nasir |
| Date Deposited: | 15 Dec 2014 03:07 |
| Last Modified: | 25 Oct 2023 04:05 |
| URI: | http://umpir.ump.edu.my/id/eprint/7623 |
| Download Statistic: | View Download Statistics |
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