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Attacks on Shen et. al.’s remote user authentication scheme and defense*
Published 2006“…We show various types of forgery attacks against Shen et. al.’s timestamp-based scheme and improve their scheme to ensure robust security for the remote authentication process keeping almost all the advantages that were present in their scheme. …”
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Proceeding Paper -
2
Span load modification via differential spoiler setting
Published 2010“…Topology of the wake vortices downstream of the configuration will largely depends on the span wise load distribution. In order to measure the span load distribution on the wing, a wake integration technique based on the control volume approach was used. …”
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Proceeding Paper -
3
Minimal spanning tree for 100 companies in Bursa Malaysia
Published 2015“…This paper investigates the stock market network among the stocks traded in Bursa Malaysia by using minimal spanning tree (MST) techniques. The daily closing prices from 2011 until 2013 of 100 companies based on market capitalization are chosen to construct the network. …”
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Article -
4
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 -
5
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 -
6
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 -
7
Empirical model of natural frequency for single span integral bridge
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Thesis -
8
Pinning for judges in harmonising Civil Law and Shariah: Challenges and prospects
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Proceeding Paper -
9
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 -
10
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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Article -
11
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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Article -
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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15
Experience, skill and competence: boundary spanning capabilities for leadership and management of transnational education
Published 2020“…Keywords: activity theory; boundary spanning distributed leadership; partnerships; professional learning community; transnational education…”
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Book Section -
16
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 -
17
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 -
18
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 -
19
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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Article -
20
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