Influences of propeller advance ratio on delta-winged uav model vortex properties by Ramalingam, Santhoshinii, Mat, Shabudin, Kasim, Khushairi Amri, Said, Mazuriah, Mohd. Nasir, Mohd. Nazri, Nik Mohd., Nik Ahmad Ridhwan, Mansor, Shuhaimi, Mohamed Radzi, Nor Haizan, Perumal, Kannan

“…The results from the surface pressure measurement have showed that the propeller advance ratio influences the development of the primary vortex above the delta-winged model. …”

Propeller locations study of a generic delta wing UAV model by Kasim, Khushairi Amri, Mat, Shabudin, Ishak, Iskandar Shah, Mansor, Shuhaimi

“…Originality/value: To the best of the author’s knowledge, the surface pressure data available for a non-slender delta-shaped UAV model is limited. …”

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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Tomography systems and sensor application for sharp-edged delta wing analysis by Bathusha, Mohamed Salman Sikandar, Mat, Shabudin, Izzuddin, Fahmi, Kasim, Khushairi Amri

“…In order to measure the vortex, a measurement technique called as surface pressure measurement was employed on the wing. …”
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