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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A comparative study of turbulence models on aerodynamics characteristics of a NACA0012 airfoil by Sadikin, Azmahani, Mohd Yunus, Nurul Akma, Abd Hamid, Saiful Anuar, Ismail, Al Emran, Salleh, Salihatun, Ahmad, Sufizar, Abdol Rahman, Mohd Nasrull, Mahzan, Shahruddin, Ayop, Sallehuddin Shah

“…This paper presented a computational fluid dynamics (CFD) simulation of air flow past a 2D model NACA0012 airfoil at high Reynolds number (Re = 3.0 x 106 ) at various angles of attack (-10 to 15). …”
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Computational fluid dynamic simulation study on NACA 4412 airfoil with various angle of attacks by Abdul Mukhti, Muhammad Ammar Qayyum, Didane, Djamal Hissein, Ogab, Mohammed, Manshoor, Bukhari

“…The aerodynamic airfoil blades have a crucial influence on the wind turbine's aerodynamic efficiency. …”
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Numerical study of wind-tunnel wall effects on lift and drag characteristics of NACA 0012 airfoil by Abobaker, Mostafa, M. Elfaghi, Abdulhafid, Addeep, Sogair

“…In this study, a numerical analysis of two-dimensional subsonic flow over a NACA 0012 airfoil at different computational domain heights, angles of attack from 0o to 10o , and operating Reynolds number of 6×106 is presented. …”
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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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The development of reynolds averaged navier stokes solver for a two dimensional compressible flow problem by M. Elkamel, Hasan Taher

“…The validation was carried out by using airfoil NACA 0012 and RAE 2822. Both two airfoils have the experimental result in terms of distribution pressure coefficient along the airfoil surfaces at different angles of attacks and Mach numbers. …”
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Investigation study of various carrier type for air tunnel transportation by Shibani, Wanis Mustafa Edukali

“…The results indicate that the carrier equipped with the airfoil NACA0012 has better performance than the carrier that uses airfoil FX 63-137 or airfoil NACA 4412 at wind speed of 30.8 m/s. …”
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Numerical simulation of aerofoil with flow injection at the upper surface by Chua, Bing Liang, Mohammed, Akmal Nizam, Sapit, Azwan, Razali, Mohd Azahari, Hushim, Mohd Faisal, Khalid, Amir, Mohd Yusof, Nurul Farhana

“…Flow around the NACA0012 airfoil was examined, with the position of flow injection jet at 90° relative to the tangential surface of the airfoil at 20%, 50% and 80% of its chord length. …”
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CFD simulation study on the performance of a modified Ram Air Turbine (RAT) for power generation in aircrafts by M. Saad, Magedi Moh, Mohd, Sofian, Zulkafli, Mohd Fadhli, Samiran, Nor Afzanizam, Didane, Djamal Hissein

“…The approach was implemented by a CRRAT system. Six airfoil profiles were tested based on 2D models and the best airfoil was chosen for implantation on the RAT and CRRAT systems. …”
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Conceptual design and multidisciplinary optimisation of power device for solar powered aircraft by Danjuma, Safyanu Bashir

“…The model was used to develop both the energy balance and mission path for Malaysia to facilitate the availability and utilisation of solar energy for successful flight operations. Airfoil analysis was conducted. WE.3.55.9.3 airfoil was the best-chosen airfoil used for the wing design, while the empennage design, NACA 0008, was the most suitable. …”
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A new direct viscous-inviscid interaction method for aerodynamics analysis by Che Mohd Husin, Mohd Faizal

“…In manner the way how to solve the flow problem past through a streamlined body such as airfoil, the present work introduce the combination of the method for solving the Euler equation and the method for solving the boundary layers equation. …”
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Parametric study on the design of baffle for three-dimensional turning diffuser by Noh @ Seth, Nur Hazirah

“…A parametric study was also conducted on the preliminary design of airfoil in determining the most optimum baffle design that is to be located inside the same turning diffuser. …”
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The effect of vortex trap on helicopter blade lift by Yaakub, Mohd Fauzi

“…In the process of designing and analyzing the grooyer, , commercial CFD, Fluent 6.3 and pre-processor Gambit were utilised in order to investigate the effect of groove which was applied on the upper surface of the helicopter airfoil. The Shear-Stress Transport (SST) k - o turbulence model was utilized in this analysis because of its capability in producing the flow inside the groove and the ability on predicting the separation of the airfoil. …”
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A High Order Compact-Flowfield Dependent Variation (HOC-FDV) method for inviscid flows by Elfaghi, A. M., Asrar, W., Omar, A. A.

“…The test cases are flow over a compression corner, a channel flow with com�pression/expansion, and a flow past NACA 0012 airfoil. The numer�ical results show an excellent agreement with analytical and pub�lished numerical results and they clearly demonstrate the higher accuracy of a single HOC-FDV scheme for both incompressible and compressible flows.…”
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