Lift Enhancement on Unconventional Airfoils by Yeung, W. W. H.

“…Lift augmentation on airfoils is a critical task to an aerodynamicist when asked to design new wings. …”
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Effectiveness of synthetic jet actuators for separation control on an airfoil by Dahalan, Md. Nizam

“…The aerodynamic performance of an airfoil could be improved by controlling flow separation using active flow control techniques. …”
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Study of mesh quality improvement for CFD analysis of an airfoil by Aqilah, F., Islam, M., Juretic, F., Guerrero, J., Wood, D., Ani, F. N.

“…Airfoils generate lift in engineering applications such as for airplanes, wind turbines, automotive spoilers, etc. …”
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Wind turbine design using thin airfoil sd2030 by Takeyeldein, M. M., Lazim, T. M., Nik Mohd., N. A. R., Ishak, I. S., Ali, E. A.

“…In this design work, the SD2030 thin airfoil was selected as a profile section for the turbine blades. …”
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Wind tunnel test to investigate transition to turbulence on wind turbine airfoil by Namin, Mahdi Hozhabri

“…The choice of the airfoils with excellent aerodynamics characteristics is an essential step in the design of wind turbine blade in order to obtain optimal performances. …”
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A Boundary Integral Method For The Planar External Potential Flow Around Airfoils by M. Murid, Ali H., S. Nasser, Mohamed M., Amin, Norsarahaida

“…Comparisons Between The Calculated And Analytical Values Of The Pressure Coefficient For The Van De Vooren Airfoil And The Karman-Trefftz Airfoil With 15% Thickness Ratio And Different Angles Of Attack Show Very Good Agreement. …”
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Enhancement on self-starting darrieus bladed wind turbine using J-shape airfoil by Rosmin, Norzanah, Yuni Rahmati, Yuni Rahmati, Evan, Ang Jun Wei, Hatib Musta'Amal @ Jamal, Aede Hatib Musta'Amal @ Jamal

“…In this paper, study has been focused to design and develop a modified-Darrieus wind turbine blade based on J-NACA0010, J-NACA0015 and J-NACA0018 airfoil profile. Performance study will be assessed in terms of its self-starting capability, tip speed ratio, angular speed and power output of the proposed system for all the above-mentioned modified airfoils. …”
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Aerodynamic noise measurement in anechoic wind tunnel of rod-airfoil with leading edge serrations by Samion, Siti Ruhliah Lizarose, Mat Ali, Mohamed Sukri

“…Turbulent flow interaction with the leading edge of an airfoil generates a well-known leading edge noise. …”
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Experimental study on flow around airfoil by using dielectric barrier discharge (DBD) plasma actuator by Zainuddin, Farah Ayiesya, Md. Daud, Nazri, Mat, Shafizal, Buntat, Zolkafle

“…This experimental study was focused on the usage of DBD plasma actuator for enhancement aerodynamic performance of airfoil model NACA 0015. The DBD plasma actuator was able to suppress flow separation near the leading edge by disturbing airflow near that region. …”
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Wind tunnel study of the effect zigzag tape on aerodynamics performance of a wind turbine airfoil by Gahraz, Seyed Reza Jafari, Mat Lazim, Tholudin, Darbandi, Masoud

“…Consequently, the tripped airfoil developed a lower pressure on the suction side in comparison to the clean airfoil. …”

Grid convergence study for detached-eddy simulation of flow over rod-airfoil configuration using openfoam by Samion, S. R. L., Shaharuddin, N. H., Mat Ali, M. S.

“…A rod-airfoil is a benchmark configuration for simulating Airfoil-Turbulence Interaction Noise (ATIN). …”
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A vortex-induced vibration-based self-tunable airfoil-shaped piezoelectric energy harvester for remote sensing applications in water by Muhammad Hafizh, Muhammad Hafizh, Muthalif, Asan G. A., Renno, Jamil, Paurobally, M. R., Mohamed Ali, Mohamed Sultan

“…This paper deals with designing, developing, and testing a nonlinear airfoil-shaped piezoelectric energy harvester from flow-induced vibration. …”
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Aerodynamic performance investigation of a small horizontal axis wind turbine with multi-airfoil blade profiles of SD2030 and E231 using wind tunnel experiments and BEM theory method. by Abu Baker, Esam Abu Baker Ali, Ishak, Iskandar Shah, Mat Lazim, Tholudin, Mohamed Takeyeldein, Mohamed, Abu Haider, Abul Bashar Mohammad

“…The rotor blade has a diameter of 0.7m and consists of two airfoils profile: the thin airfoil SD2030 selected at the outboard region, and the thick airfoil E231 at the inboard region. …”
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Effect of surface roughness on drag of loggerhead carapace by Kah Poh, Alan Chan, Yuan, Cheng See, Mat Yamin, Ahmad Kamal, Jalaluddin, Ainil Jesita, Ishak, Iskandar Shah, Mansor, Shuhaimi

“…The pressure coefficient, Cp distribution across the Loggerhead carapace was also investigated and is compared to the Cp trend of an airfoil in order to deduce the aerodynamics features of the Loggerhead carapace. …”
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Diffuser augmented wind turbine for low-speed wind by Elsherbeiny, Mohamed Mohamed Takeyeldein

“…The design of DAWT was developed by designing a bare wind turbine and a diffuser suitable for low wind speeds. The thin airfoil SD2030 was used as the blade profile of the bare turbine, while the suction surface of the same airfoil was also used as the profile of the diffuser to overcome laminar separation. …”
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An integral equation for the external potential flow problem by Murid, Ali Hassan Mohamed, Nasser, Mohamed M. S., Saidina Amin, Norsarahaida

“…It is shown that the integral equation obtained is still valid if the obstacle is an airfoil without a cusp trailing edge. The integral equation is solved using the Nystrom. …”

Aerodynamic characteristics of compound wing configuration of wing-in-ground effect vehicle by Jamei, Saeed

“…The compound wing was divided into three parts where one rectangular wing in the middle and two reverse taper wings with anhedral angle at the sides. NACA6409 airfoil was selected as a case study for the wing airfoil section. …”

A boundry integral equation for the 2D external potential flow by Nasser, M., Mohamed Murid, Ali Hassan, Saidina Amin, Norsarahaida

“…Comparisons between numerical and analytical values of the pressure coefficient on the surface of the NACA 0009 and NACA 0012 airfoils with zero angle of attack show a very good agreement…”
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Computational fluid dynamic on double delta wing by Abd. Halim, Khairul Adzha, Mat, Shabudin

“…Basic concept of aircraft wing design is based on airfoil section. Time flies, evolution in aircraft wing design shows the desire of mankind to improve the speed, agility, maneuverability of an aircraft. …”

Performance characteristics of generic bell 206b helicopter tail rotor blade using empirical numerical method by Mahamad, Firdaus, Koto, Jaswar, Ishak, Iskandar Shah, Ammoo, Mohd. Shariff

“…This paper presents the Empirical Numerical Method for the analysis of the performance characteristics of a generic bell 206B helicopter tail rotor blade. The airfoil profile of the blade is near similar to NACA 0012 series, with maximum thickness 12% at 33% chord. …”