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Spikes blocking and surge protection
Published 2011“…In order to ensure a constant voltage source, we employ line regulation, load regulation and ripple rejection. …”
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Book Chapter -
2
Real time astrocyte in spiking neural network
Published 2015“…In this paper, a novel model for (ANGN) is proposed to model the real time interaction between Astrocytes and neurons by using Spiking Neural Networks (SNNs) and mathematical models for astrocyte-neuron interaction. …”
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Proceeding Paper -
3
Encoding of facial images into illumination-invariant spike trains
Published 2012“…Some previous work of several researchers have mathematically proven the advantage of Spiking Neural Network (SNN) in term of computational power and one of the neuron model that shows promising result is Spike response Model (SRM). …”
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Proceeding Paper -
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Numerical investigation of the vortical flow over delta wing and reverse delta wing
Published 2012“…This study aims to give some thoughts and initial understanding of passive wake vortex alleviation by introducing add-ons devices onto the aircraft, which are delta wing (DW) and reverse delta wing (RDW). However, as a preliminary investigation, the study has treated these devices separately from the aircraft in order to clearly visualize the wake vortex formation behind the wing as a standalone. …”
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Proceeding Paper -
6
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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Article -
7
Recognizing faces with normalized local Gabor features and Spiking Neuron Patterns
Published 2016“…{SNP} is acquired from projection of LGFV//LN features using Spike Response Model (SRM), a neuron model describing the spike behavior of a biological neuron. …”
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Article -
8
Study of the reverse delta wing
Published 2011“…A six-component balance was used to obtain the aerodynamic coefficients for a reverse delta wing as well as a delta wing for comparison. A simulation of the streamlines, velocity vectors, and surface pressure contours was carried out using computational fluid dynamics software to show the characteristics of the flow over a reverse delta wing.…”
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Article -
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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 -
12
Pin type reconfigurable clamping ability evaluation for setup-free technology
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Book Chapter -
13
An experimental study on precision grinding of silicon using diamond grinding pins
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Article -
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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 -
16
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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Article -
17
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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Article -
18
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 -
19
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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Article -
20
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