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Primary ewing's sarcoma of the lumbosacral spine : a case report
Published 2012“…Intraoperative finding was an extradural mass from L3-L5 with extension to bilateral neuroforamen. Histopathology report defined a round cell tumour of Ewing's sarcoma from the mass.…”
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Numerical investigation of the vortical flow over delta wing and reverse delta wing
Published 2012“…It is also observed that delta wing (DW) generates stronger wake vortices with greater peak velocity than the wake vortices generated by reverse delta wing (RDW)…”
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Proceeding Paper -
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Assessment of growth monitoring among children younger than 5 years at early childhood development centres in Nelson Mandela Bay, South Africa
Published 2024“…Results showed that 13.1% (n = 214) were stunted by height for age Z‐score (HAZ < −2) and 4.5% (n = 74) were severely stunted (HAZ < −3). The prevalence of moderate acute malnutrition was 1.2% and severe acute malnutrition was 0.5%, while the prevalence of overweight was 9.2% and the prevalence of obesity was 4%. …”
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Optimum length for pin fins used in electronic cooling
Published 2012“…The present work deals with the heat transfer analysis of pin fins of various geometries namely ─ circular, triangular and rectangular and thus arrive at the optimum design. …”
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Study of the reverse delta wing
Published 2011“…Particle image velocimetry was used in a low-speed wind tunnel to investigate the vortex structures of a slender reverse delta wing at various angles of attack and roll. This work investigates the characteristics of the vortices generated downstream in planes perpendicular to the freestream direction and their dependence on angles of attack and roll at a chord-based Reynolds number of Rec= 382000 The peak tangential velocities at�angle of attack higher than 5 deg show a trend similar to a delta wing. …”
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Pinning for judges in harmonising Civil Law and Shariah: Challenges and prospects
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Proceeding Paper -
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Experimental investigation of wing tip vortex
Published 2009“…Particle image velocimetery was used in a low-speed wind tunnel to investigate and characterize wing tip vortex structures. A rectangular wing of a SWIM model was used as a vortex generator in two different configurations, (i) plain wing and (ii) flapped wing with trailing edge flap extended at 20 degrees. …”
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Proceeding Paper -
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Ethnoichthyology of the First Record of Spine Bahaba (Bahaba polykladiskos) from Muar, Johor, Malaysia
Published 2024“…The Spine Bahaba (Bahaba polykladiskos), locally known as 'Gelama Tirusan,' is a member of the Sciaenidae fish family that is distributed across Southeast Asia, reaching as far as North Australia. …”
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Pin type reconfigurable clamping ability evaluation for setup-free technology
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Book Chapter -
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An experimental study on precision grinding of silicon using diamond grinding pins
Published 2011Get full text
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More than human aesthetics: interactive enrichment for elephants
Published 2020“…Applying existing aesthetic dimensions and design principles to the challenge of designing interactive enrichment for them, we show how the insights gained can inform more than human centered design in different settings. …”
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Conference or Workshop Item -
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Right-wing populism and religion in Europe and the USA
Published 2020“…The aim of this paper is to examine comparatively the growth and political effectiveness of right-wing populism in Western Europe, Central Europe, and the USA since 9/11. …”
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Flutter analysis of supersonic wing with external stores
Published 2013“…In the present paper, the simulation of supersonic wing equipped with external loads of missiles on the wing had been analyzed at high supersonic region. …”
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Proceeding Paper -
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NFC based attendance: more than just a touch
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Proceeding Paper -
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5.5-10.5 GHz IR-UWB Pulse Generator for Narrowband Interference Mitigation
Published 2012“…An impulse radio ultra wideband (IR-UWB) pulse generator works between 5.5-10.5 GHz for narrowband interference mitigation is proposed. …”
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Proceeding Paper -
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Experimental investigation of free wing IIUM-UAV configuration
Published 2010“…In this work, the IIUM first free wing unmanned aerial vehicle model (IIUM-FWUAV) was investigated experimentally. …”
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Proceeding Paper -
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Oscillating supersonic delta wing with straight leading edges
Published 2012“…A Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with straight leading edge for the attached shock case. …”
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Effect of angle of incidence on stability derivatives of a wing
Published 2014“…In the Present paper effect of angle of incidence on pitching derivatives of a delta wing with curved leading edges of a attached shock case is been studied. …”
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Article