01984nam a2200241 a 4500 vtls000078519 KUKTEM 20251114204613.0 140523t2013 my a f m 000 0 eng d THE0006960(Local) 201906131227 aida 201603311102 huda 201405231126 training4 UMP TK7872.M25 H34 2013 rs Bc. Muhammad Hafizuddin Ismail Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number / Muhammad Hafizuddin Ismail Kuantan, Pahang : UMP, 2013 xiii, 29 p. : ill. (some col.) ; 30 cm. + 1 CD-ROM Project paper (Bachelor of Mechatronics Engineering) -- Universiti Malaysia Pahang -- 2013 Bibilography : p. 29 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. Aerodynamic airfoil 0 0 0 1 20000 20000 2019-09-04 0 TK7872.M25 H34 2013 rs Bc. 0000080260 2019-09-04 00:00:00 1 2019-09-04 PSM 0 0 0 1 20000 20000 2019-09-04 0 CD 7737 | TK7872.M25 H34 2013 rs Bc. 0000080261 2019-09-04 00:00:00 1 2019-09-04 PSM VIRTUA40 4912 4918 VTLSSORT0080*0200*0400*0900*1000*2450*2600*3000*5020*5040*5200*6500*9992