-
1
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. …”
Get full text
Proceeding Paper -
2
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. …”
Get full text
Article -
3
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.…”
Get full text
Article -
4
Pinning for judges in harmonising Civil Law and Shariah: Challenges and prospects
Published 2009Get full text
Get full text
Proceeding Paper -
5
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. …”
Get full text
Get full text
Proceeding Paper -
6
Pin type reconfigurable clamping ability evaluation for setup-free technology
Published 2011Get full text
Book Chapter -
7
An experimental study on precision grinding of silicon using diamond grinding pins
Published 2011Get full text
Article -
8
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. …”
Get full text
Get full text
Proceeding Paper -
9
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. …”
Get full text
Article -
10
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. …”
Get full text
Get full text
Article -
11
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. …”
Get full text
Proceeding Paper -
12
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. …”
Get full text
Article -
13
Flow visualization over a circular planform wing
Published 2013“…circular plan form wing at high Reynolds numbers has been carried out numerically. …”
Get full text
Get full text
Proceeding Paper -
14
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. …”
Get full text
Article -
15
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. …”
Get full text
Article -
16
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. …”
Get full text
Article -
17
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. …”
Get full text
Article -
18
Evaluation of aircraft wing-tip vortex using PIV
Published 2009“…The formation and development of a wing-tip vortex in a near and extended near filed were studied experimentally. …”
Get full text
Proceeding Paper -
19
Firearm recognition based on whole firing pin impression image via backpropagation neural network
Published 2011“…Firearms identification is a vital aim of firearm analysis. The firing pin impression image on a cartridge case from a fired bullet is one of the most significant clues in firearms identification. …”
Get full text
Book Chapter -
20
Firearm recognition based on whole firing pin impression image via backpropagation neural network
Published 2011“…Firearms identification is a vital aim of firearm analysis. The firing pin impression image on a cartridge case from a fired bullet is one of the most significant clues in firearms identification. …”
Get full text
Proceeding Paper