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161
Wideband and multiband antennas for multi-configuration mode applications
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Thesis -
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Novel opto-electronic and plastic fibre sensors
Published 1998“…The middle POF is coupled to a red LED and emits light onto a flat target with the two outer fibres receiving the reflected light from the target and guiding it to two silicon PIN photodiodes. Theoretical investigations on the behaviour of the sensor are presented for ranges between 0 mm and 100 mm, and for targets with different reflectivities. …”
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Thesis -
165
Evolution of NACA23012 wake vortices structure using PIV
Published 2012“…The formation and development of a wing‐tip vortex in a near and extended near field were studied experimentally. …”
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Article -
166
Design of a planar structure of multifrequency patch antenna
Published 2008“…The proposed antenna structure comprises a center patch antenna known as driven patch and two adjacent microstrip patches defined as wing patches. The effect of gap between driven patch and the wing patches have been studied for multiband frequency operation. …”
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Article -
167
Tool wear during milling laminated carbon fibre reinforced plastic
Published 2015“…It is observed that the wear area is found polished and shining which is due to the abrasive nature of the carbon. …”
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168
Span load modification via differential spoiler setting
Published 2010“…The serious impact of the wing tips vortices of a large aircraft is well known. …”
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Proceeding Paper -
169
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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Untitled (Publicity notice board)
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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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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 -
180
Serpentine microfluidic structures for concentration rradient generators
Published 2016Get full text
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Proceeding Paper