Effectiveness of synthetic jet actuators for separation control on an airfoil by Dahalan, Md. Nizam

“…The unsteady aerodynamic loads were calculated from the surface pressure measurements of 30 ports along the wing chord for both upper and lower surfaces. …”
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Wind tunnel experiments on a generic sharp-edge delta wing UAV model by Mohd. Zain, Nadhirah, Mat, Shabudin, Kasim, Khushairi Amri, Mansor, Shuhaimi, Dahalan, Md. Nizam, Othman, Norazila

“…During the experiments, two measurement techniques were employed; steady forces and surface pressure measurements. The experimental data highlights an impact of propeller size on the coefficients of lift, drag, and moment and vortex system of the delta-shaped UAV. …”
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Experimental investigation on blunt-edged UTM delta wing VFE-2 configurations at low reynolds number by Daman Huri, Muhammad Zal Aminullah, Mat, Shabudin, Said, Mazuriah, Mansor, Shuhaimi, Dahalan, Md. Nizam, Abdul-Latif, Ainullotfi

“…Two measurement techniques were employed on the upper surface of the wing, i.e. experimental surface pressure and tuft techniques. Experiments were also conducted on two different leading edge profiles namely medium and large radius profiles with different leading edge radius-to-wing chord ratio. …”

Wind tunnel experiment of UTM-LST generic light aircraft model with external store by Abdul Manaf, Muhammad Zaki, Mat, Shabudin, Mansor, Shuhaimi, Nasir, Mohd. Nazri, Mat Lazim, Tholudin, Wan Ali, Wan Khairuddin, Wan Omar, Wan Zaidi, Mohd. Ali, Zurriati, Abdul-Latif, Ainullotfi, Abd. Wahid, Mastura, Dahalan, Md. Nizam, Othman, Norazila

“…An interesting feature observed from surface pressure studies where, the results showed that the pressure coefficient increased when the external is mounted on the wing at a low angle of attack. …”