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## Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil

#### Robiul Islam Rubel [1] , Md. Kamal Uddin [2] , Md. ZAHİDUL ISLAM [3] , Md. Rokunuzzaman [4]

An aerofoil is stream line body. Symmetric aerofoil (NACA 0015) is used in many applications such as in aircraft submarine fins, rotary and some fixed wings. The ultimate objective of an aerofoil is to obtain the lift necessary to keep an airplane in the air. But construction of the blade with proper angle of attack and implementation has significant effect on lift force. Insufficient lift force might cause fail of airplane flying, especially at high speed. Modern technologist use different simulation techniques to avoid costly model testing. But simulation is based on some assumption. Thus practically results are not fully authentic and have a deviation. In this work numerical and experimental investigation of NACA 0015 is studied at different angle of attack (degree) at different velocity of air by determining the forces at every two degrees from 00 to 180. The experimental is conveyed in a low speed wind tunnel. The numerical analysis is conducted using ANSYS (combined with CFD and FLUENT FLOW). The use of the CFD technology greatly reduces the overall investment and efforts for aerofoil design. CFD method contributes to visualize the flow pattern inside aerofoil and takes less time and faster according to experimental methods. After completing the experimental and numerical data is compared. Therefore objective of this paper is to find the deviation and validation of aerodynamics characteristics of aerofoil NACA 0015 for experimental and numerical method.
CFD Fluent Flow, Lift and Drag Force, Experimental analysis, Numerical analysis
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Subjects Engineering Articles Author: Robiul Islam Rubel Institution: BOZOK ÜNİVERSİTESİ, TIP FAKÜLTESİ, CERRAHİ TIP BİLİMLERİ BÖLÜMÜ, GENEL CERRAHİ ANABİLİM DALICountry: Bangladesh Author: Md. Kamal Uddin Institution: Rajshahi University of Engineering & TechnologyCountry: Bangladesh Author: Md. ZAHİDUL ISLAM Institution: Rajshahi University of Engineering & TechnologyCountry: Bangladesh Author: Md. Rokunuzzaman Institution: Rajshahi University of Engineering & TechnologyCountry: Bangladesh Publication Date : April 20, 2017
 Bibtex @research article { ijet280499, journal = {International Journal of Engineering Technologies IJET}, issn = {2149-0104}, eissn = {2149-5262}, address = {}, publisher = {İstanbul Gelisim University}, year = {2017}, volume = {2}, pages = {132 - 141}, doi = {10.19072/ijet.280499}, title = {Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil}, key = {cite}, author = {Islam Rubel, Robiul and Kamal Uddin, Md. and Zahi̇dul Islam, Md. and Rokunuzzaman, Md.} } APA Islam Rubel, R , Kamal Uddin, M , Zahi̇dul Islam, M , Rokunuzzaman, M . (2017). Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil . International Journal of Engineering Technologies IJET , 2 (4) , 132-141 . DOI: 10.19072/ijet.280499 MLA Islam Rubel, R , Kamal Uddin, M , Zahi̇dul Islam, M , Rokunuzzaman, M . "Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil" . International Journal of Engineering Technologies IJET 2 (2017 ): 132-141 Chicago Islam Rubel, R , Kamal Uddin, M , Zahi̇dul Islam, M , Rokunuzzaman, M . "Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil". International Journal of Engineering Technologies IJET 2 (2017 ): 132-141 RIS TY - JOUR T1 - Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil AU - Robiul Islam Rubel , Md. Kamal Uddin , Md. Zahi̇dul Islam , Md. Rokunuzzaman Y1 - 2017 PY - 2017 N1 - doi: 10.19072/ijet.280499 DO - 10.19072/ijet.280499 T2 - International Journal of Engineering Technologies IJET JF - Journal JO - JOR SP - 132 EP - 141 VL - 2 IS - 4 SN - 2149-0104-2149-5262 M3 - doi: 10.19072/ijet.280499 UR - https://doi.org/10.19072/ijet.280499 Y2 - 2017 ER - EndNote %0 International Journal of Engineering Technologies Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil %A Robiul Islam Rubel , Md. Kamal Uddin , Md. Zahi̇dul Islam , Md. Rokunuzzaman %T Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil %D 2017 %J International Journal of Engineering Technologies IJET %P 2149-0104-2149-5262 %V 2 %N 4 %R doi: 10.19072/ijet.280499 %U 10.19072/ijet.280499 ISNAD Islam Rubel, Robiul , Kamal Uddin, Md. , Zahi̇dul Islam, Md. , Rokunuzzaman, Md. . "Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil". International Journal of Engineering Technologies IJET 2 / 4 (April 2017): 132-141 . https://doi.org/10.19072/ijet.280499 AMA Islam Rubel R , Kamal Uddin M , Zahi̇dul Islam M , Rokunuzzaman M . Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil. IJET. 2017; 2(4): 132-141. Vancouver Islam Rubel R , Kamal Uddin M , Zahi̇dul Islam M , Rokunuzzaman M . Numerical and Experimental Investigation of Aerodynamics Characteristics of NACA 0015 Aerofoil. International Journal of Engineering Technologies IJET. 2017; 2(4): 132-141.

Authors of the Article
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