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The Potts model with countable set of spin values on a Cayley tree
Published 2006“…We consider a nearest-neighbor Potts model, with countable spin values 0, 1, . . .,and non zero external field, on a Cayley tree of order k (with k+1 neighbors). …”
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Limiting Gibbs measures of Potts model with countable set of spin values
Published 2007“…We consider a nearest-neighbor Potts model, with countable spin values Φ = {0, 1, . . .}, and nonzero external field, on a Cayley tree of order k (with k + 1 neighbors). …”
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Spin squeezing as a measure of entanglement in a two-qubit system
Published 2003“…The relationship between entanglement and spin squeezing parameters in the two-atom Dicke system was examined. …”
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New record of Cochlodiniam SP.in Perak coastal water of Peninsular Malaysia
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Letter to J J Long
Published 1939“…Typescript letter informing Mr Long of recent developments. Unsigned. Dated 20 January 1939.…”
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Letter to J J Long
Published 1939“…Typescript letter dated 20 March 1939, from the Organising Secretary of the Anti-Partition of Ireland League to J J Long, about an upcoming meeting in the Clapham area.…”
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Development of educational software for stress analysis of an aircraft wing
Published 2012“…The developed software can be used to estimate load on a wing and to compute the stresses at any point along the span of the wing of a given aircraft. …”
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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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Oscillating supersonic delta wings 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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Oscillating supersonic delta wings with curved leading edges
Published 2010“…In the present study Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for the attached shock case. A strip theory is used in which strips at different span-wise locations are independent. …”
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Experimental investigation of plain- and flapped-wing tip vortices
Published 2009“…Particle image velocimetry was used in a low-speed wind tunnel to investigate and characterize wing tip vortex structures. A rectangular wing of a subsonic wall interference model was used as a vortex generator in two different configurations: 1) plain wing and 2) flapped wing with the trailing-edge flap extended at 20 degrees. …”
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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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Flow visualization over a circular planform wing
Published 2013“…circular plan form wing at high Reynolds numbers has been carried out numerically. …”
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Proceeding Paper