Computation of airfoil boundary layer by Nurfhaizatul Aqma, Chik Aik

“…Computation of Airfoil boundary layer is an analysis of flow around an airfoil using a CFD commercial packages, GAMBIT/FLUENT. …”
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Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet by Djojodihardjo, H., M. F., Abdul Hamid, Abdul Aziz, Jaafar, Shah Nor, Basri, F. I., Romli, F., Mustapha, A. S., Mohd Rafie, D. L. A., Abdul Majid

“…A trade-off study on the S809 Coanda configured airfoil is needed to judge the optimum configuration of Coandă-jet fitted Wind-Turbine design.…”
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Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number by Muhammad Hafizuddin, Ismail

“…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. …”
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A study of drag force on different type of airfoil in a subsonic wind tunnel by Muhamad Faruqi, Zahari

“…There had been a number of researches that investigated on drag force of airfoil in subsonic wind tunnel. This study was then conducted in order to identify drag force in subsonic wind tunnel using Computational Fluid Dynamics (CFD) software. …”
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Airfoil selection and computational study on the torque performance of 4-blade vertical axis wind turbine by Sunny, Kalakanda Alfred, Kumar, Pradeep, Kumar, Nallapaneni Manoj, Banerjee, Joy, Adheena, G.J.

“…NACA0012, NACA0015, NACA0018 and NACA0021 airfoil types were analysed for the tangential force they create at different angle of attack. …”
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Effect of Stall Strip Position, Size and Geometry on the Lift Coefficient of NACA 001 Aerofoil by Wee, Tee, A. N., Oumer, Ahmmad, Shukrie, Azizuddin, Abdul Aziz, Baheta, Aklilu

“…This study aims to determine the optimum position and geometry of stall strips (SS) to control sudden fall of lift in wind turbine blades. The type of airfoil used in this study is NACA 0015 with 150 mm of chord length. …”
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Design and evaluation of the empennage for reconnaissance UAV by Izzan Hairi, Mohd Ibrahim

“…This report also contains the analysis of the airfoil and finally the design of the empennage and the UAV will be done by CAD software.…”
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The analysis of wing performance for reconnaissance UAV by Zulkifli, Yusof

“…To avoid this problem, it is important to calculate where to put the wing onto the fuselage and which airfoil should be used for the wing. If the selection are made carelessly, the UAV probably cannot fly or can fly but in a bad condition. …”
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Two blade vertical axis wind turbine: investigations on the torque generation at different rotational velocities by Sunny, Kalakanda Alfred, Kumar, Pradeep, Kumar, Nallapaneni Manoj, Veena, A., G. J., Adheena

“…This study includes the selection of airfoil by comparing lift and drag generated by airfoils NACA 0012, NACA 0015, NACA 0018, and NACA 0021. …”
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CFD-study of the H-Rotor Darrius wind turbine performance in drag-lift and lift regime : Impact of type, thickness and chord length of blades by Ghiasi, Pedram, Najafi, Gholamhassan, Ghobadian, Barat, Jafari, Ali, Rizalman, Mamat, Mohd Fairusham, Ghazali

“…Increasing the thickness from 18 to 22 % of chord length exerts a negative influence on the turbine's performance in both regimes, and at lower TSRs, NACA0018 airfoil with a chord length of 0.2 m was of the optimum performance in the drag-lift regime.…”
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