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Design, fabrication and experimental testing of IIUM free wing unmanned aerial vehicle (IIUM-FWUAV)
Published 2011“…In this work, IIUM’s first free wing unmanned aerial vehicle model (IIUM-FWUAV) was designed, fabricated, tested and investigated experimentally. …”
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127
DNA Test of paternity in Islamic Law: Implications for children born less than minimum gestation period in Malaysia
Published 2016“…The Problem of children born within the marriage but less than six months is a disputed issue in Islamic law. …”
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Pitch and roll derivatives of a delta wing with curved leading edge in high speed flow
Published 1990“…Ghosh's unified similitude has been applied to oscillating delta wings of arbitrary plan forms in supersonic/ hyper- sonic flow. …”
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Impact of a reverse delta type add-on device on the flap-tip vortex of a wing
Published 2016“…The effect of interactions of vortices produced by an outboard flap-tip of a half-span wing (NACA 23012 in landing configuration) and a slender reverse delta type add-on device, placed in the proximity of the outboard flap-tip, on the upper surface of the half-span wing is investigated using Particle Image Velocimetry in a closed loop low speed wind tunnel. …”
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A high-gain quasi-fractal antenna with wide range operation for 5G applications over V-band spectrum
Published 2022“…The antenna is shown to provide an average gain exceeding 6.5 dBi across 59 GHz to 68 GHz. The simple geometrical configuration of the antenna and its radiation characteristics makes it a potential candidate for 5G applications operating in V-band.…”
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Enhancement of analyte atomic lines with excitation energies of about 5 eV in the presence of molecular gases in analytical glow discharges
Published 2014“…Small amounts of hydrogen or oxygen in either argon or neon plasmas cause previously unexplained enhanced excitation of various analyte atomic lines with upper energies close to 5 eV. We suggest this enhancement is due to three body collisions involving two hydrogen or oxygen atoms and a sample atom.…”
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First five decisions of the European Court with respect to the Republic of Armenia
Published 2006“…Narine Gasparyan discusses the first 5 European Court decisions concerning Armenia…”
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Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge
Published 2015“…For Mach number M = 2, this limiting value of validity is fifteen degrees, for Mach 2.5 & 3, it is twenty five degrees, whereas, for Mach 3.5 & 4 it becomes thirty five degrees, when these stability derivatives were considered at various pivot positions; namely at h = 0.0, 0.4, 0.6, and 1.0. …”
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What helps children learn difficult tasks: a teacher's presence may be worth more than a screen
Published 2019“…Conversely, physically taking part in interactive touchscreen training did not result in more learning than passive screen viewing.…”
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LL5 directs the translocation of Filamin A and SHIP2 to sites of phosphatidylinositol 3,4,5-triphosphate (PtdIns(3,4,5)P3) accumulation, and PtdIns(3,4,5)P3 localization is mutually modified by co-recruited SHIP2
Published 2010“…Phosphatidylinositol 3,4,5-triphosphate (PtdIns(3,4,5)P3) accumulates at the leading edge of migrating cells and works, at least partially, as both a compass to indicate directionality and a hub for subsequent intracellular events. …”
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Rights in psychiatric care : implementation of Shtukaturov v Russia
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Why the processing of repeated targets are better than that of no repetition: evidence from easy-to-difficult and difficult-to-easy switching situations
Published 2014“…Background: Previous studies have found that the processing of repeated targets are easier than that of non-repetition. Although several theories attempt to explain this issue, the underlying mechanism still remains uncovered. …”
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Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)
Published 2011“…Result of the outboard loading case 2 shows a limited effect in terms of the wing tip vortex structure. This can be due to the relatively large separation distance between the wing tip and the deployed spoilers, preventing the spoiler wake/wing tip vortex interaction in the near field.…”
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