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141
Investigation of aerodynamic parameters of a hybrid airship
Published 2012“…The aerodynamic parameters of a preliminary winged-hull airship design are investigated. The research methodology involved the use of numerical simulation and wind tunnel testing. …”
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142
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143
Untitled (Publicity notice board)
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Photograph -
144
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Investigation of Empennage Location Effect to the Unmanned Aerial Vehicle (UAV) Structure Characteristic
Published 2024“…Interestingly, the hybridization of fixed-wing and rotary UAV gives better performance in terms of energy consumption and the needs of runaway. …”
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149
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151
Design, build and test IIUM remote controlled glider
Published 2010“…NACA 4412 airfoil was used for the wing sectiion. The fuselage diensions were estimated. …”
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Proceeding Paper -
152
Serpentine microfluidic structures for concentration rradient generators
Published 2016Get full text
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Proceeding Paper -
153
Numerical investigation of the effect of spoiler’s configuration on wake vortex
Published 2012“…A numerical investigation was undertaken to study the aerodynamic characteristics of wake vortices generated from an aircraft during taking-off or landing, and thus exploring the possible techniques of reducing hazard imposed to the following aircraft by means of passive wake vortex alleviation by using delta wing (DW) as an add-on device. Simulations were performed using RANS turbulence model.…”
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Monograph -
154
Influence of differential spoiler settings on the wake the vortex characterization and alleviation
Published 2010“…Experimental investigations using particle image velocimetry technique have been carried out for the evaluation of the differential spoiler setting capabilities in modifying the spanwise wing load and further reduce the wake vortex hazard. …”
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155
Influence of differential spoiler settings on the wake vortex characterization and alleviation
Published 2010“…Experimental investigations using particle image velocimetry technique have been carried out for the evaluation of the differential spoiler setting capabilities in modifying the spanwise wing load and further reduce the wake vortex hazard. …”
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156
Development of the IIUM hybrid airship
Published 2010“…In this paper, the preliminary design steps of a winged hull hybrid airship will be outlined and discussed together with a way to achieve controllability of the hybrid airship during both STOL (Short take off and Landing) and cruising mode as well as its aerodynamic characteristics.…”
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Proceeding Paper -
157
Book review : The people vs. democracy: why our freedom is in danger and how to save it / by Yascha Mounk
Published 2019“…Trump, who he identifies unequivocally as a right-wing populist. If there is one thing guaranteed to make liberal democrats sit up and take notice it is the idea that the United States, for many a venerable bastion of liberal democracy, is now part of a new and highly unexpected populist landscape.…”
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Reconfigurable patch antenna by RF MEMS switches
Published 2009“…The proposed antenna structure comprises a center patch antenna known as driven patch and two adjacent microstrip patches defined as wing patches. Cantilever MEMS bridges are introduced to provide to operate antenna either 21.73 GHz or 23.6 GHz depending on the position of the MEMS switches. …”
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Proceeding Paper