The effects of vortex shedding on the aerodynamic performance of airfoils by Sikien, Esther Rami, Abdullah, Aslam, Zulkafli, Mohd Fadhli, Rahim, Mohammad Zulafif

“…This is a comparative study involving various National Advisory Committee for Aeronautics (NACA) airfoils NACA 0012, NACA 0024, NACA 4412 and NACA 4424. …”
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Comparative study of turbulent incompressible flow past naca airfoils by Abdullah, Aslam, Roslan, Amirul Aizad, Omar, Zamri

“…The flow past the airfoils is continuously investigated in various experimental and computational aerodynamic perspectives. …”
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Numerical study of the flow over symmetrical airfoils with ground effects by Abdullah, Aslam, Suresh, Surendran, Mohd Saleh, Siti Juita Mastura, Zulkafli, Mohd Fadhli, Abdul Ghafir, Mohammad Fahmi

“…The paper presents the ground effects on the flow over five NACA symmetrical airfoils by analyzing the coefficients of lift. The unbounded flow over a selected airfoil was first simulated, and the results were validated against the established data in order to validate the method used in obtaining the lift coefficients. …”
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Selig airfoils: topology of flow patterns at low reynolds number by Che Ibrahim, Che Intan Hartini, Abdullah, Aslam

“…Despite a clear methodology, such flow topology studies have not yet covered the majority of airfoil types. This study considers three low Reynolds number Selig airfoils. …”
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Flow topology around low reynolds number airfoils with vortex shedding by Che Ibrahim, Che Intan Hartini, Abdullah, Aslam

“…While the topology methodology is quite well established, the majority of airfoil types have still not been covered. In this study, six low Reynolds number airfoils were considered to investigate the separation bubble structure, vortex shedding and reattachment point. …”
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Vortex formation in unsteady flow over NACA 4412 and NACA 4424 airfoils by Hadi, Muhammad Irfan, Nazri, Mohd., Abdullah, Aslam

“…Over the years, the effects of vortex formation on the aerodynamic performance of airfoils have served as motivation for many research studies. …”
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Flow topology around low reynolds number eppler airfoils with vortex shedding by Che Ibrahim, Che Intan Hartini, Abdullah, Aslam, Razali, Mohd. Azahari

“…The results are useful in micro aerial vehicles application where the airfoils are those of low Reynolds number.…”
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Comparative study of two dimensional boundary layer over NACA 23012 and NACA 23021 airfoils by using keller’s box method by Kumar, Vinod Kumar K Sivak, Abdullah, Aslam, Basuno, Bambang

“…This study aims at utilising a developed computer code which allows one to predict the development of boundary layer characteristics along airfoils’ surface, and have a comparative understanding on flow behaviours between NACA 23012 and NACA 23021 airfoils, as well as 0⁰ and 5⁰ angles of attack. …”
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