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Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
Published 2010“…This research focused on the design, construction and testing of a free wing remote controlled aerial vehicle. The free wing concept allows the wing to move freely in pitch relative to the fuselage. …”
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Proceeding Paper -
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Effect of angle of incidence on roll damping derivatives of a delta wing
Published 2014“…In the Present paper effect of angle of incidence on roll damping derivative of a delta wing with curved leading edges with attached shock case has been studied. …”
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Feasibility of QKD over FSO Link
Published 2012“…QKD is possible over fiber cable and Free Space Optical (FSO) links. Fiber based QKD may be used if direct line of sight link is not possible, but it brings along many problems related to material properties of fiber cable and detector limitations. …”
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Speaker on " 5 characteristics of excellent Muslims women" (5 ciri wanita Islam cemerlang)
Published 2011Get full text
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The development of a fixed wing aircraft analysis and design flight dynamic software
Published 2016“…Through the implementation of five types of aircraft models, the developed computer code represents a useful tool for flight dynamic analysis and control design for a fixed-wing aircraft.…”
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Stability assessment of 132kV Sabah grid-connected solar pV system
Published 2014“…Therefore in this project, system study will be carried out to determine the largest possible capacity of Photovoltaic (PV) solar power generation to be injected to the Northern Grid of SESB’s 132kV network.The system study was first carried out by injection of 25MW of solar PV plant and the result showed some violation in the transformer at 275/132kV Segaliud substation. …”
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Calcification of the alar ligament mimics fracture of the craniovertebral junction (CVJ): an incidental finding from computerised tomography of the cervical spine following trauma
Published 2009“…However, if further imaging and evaluation of the cervical spine with computerised tomography (CT) did not demonstrate an obvious fracture, then the possibility of ligament calcification would be considered. …”
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Drag analysis of an aircraft wing model and without bird feather like winglet
Published 2012“…The model of the rectangular wing with bird feather like winglet has been fabricated using polystyrene before design using CATIA P3 V5R13 software and finally fabricated in wood. …”
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Numerical simulation of a low aspect ratio wing at low Reynolds number
Published 2013“…In this work the numerical simulation of aerodynamic performance of low aspect ratio wings at low Reynolds numbers applicable to micro aerial vehicle is carried out. …”
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Proceeding Paper -
55
Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
Published 2016“…Aerostatic lift in a hybrid buoyant aircraft reduces the wing loading as well as the induced drag. This reduction is valid till pressure height. …”
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Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
Published 2012“…In the present study hypersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with curved leading edges for the attached shock case. …”
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Stability derivatives of a delta wing with straight leading edge in the Newtonian limit
Published 2013“…They are applicable for wings of arbitrary plan form shape at high angles of attack provided the shock wave is attached to the leading edge of the wing. …”
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