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Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
Published 2010“…This research focused on the design, construction and testing of a free wing remote controlled aerial vehicle. The free wing concept allows the wing to move freely in pitch relative to the fuselage. …”
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Proceeding Paper -
22
Drag analysis of an aircraft wing model and without bird feather like winglet
Published 2012“…This work describes the aerodynamic characteristic for aircraft wing model with and without bird feather like winglet. …”
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Article -
23
Numerical simulation of a low aspect ratio wing at low Reynolds number
Published 2013“…In this work the numerical simulation of aerodynamic performance of low aspect ratio wings at low Reynolds numbers applicable to micro aerial vehicle is carried out. …”
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Proceeding Paper -
24
Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
Published 2016“…Aerostatic lift in a hybrid buoyant aircraft reduces the wing loading as well as the induced drag. This reduction is valid till pressure height. …”
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Article -
25
Stability derivatives of a delta wing with straight leading edge in the Newtonian limit
Published 2013“…They are applicable for wings of arbitrary plan form shape at high angles of attack provided the shock wave is attached to the leading edge of the wing. …”
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26
The development of a fixed wing aircraft analysis and design flight dynamic software
Published 2016“…Through the implementation of five types of aircraft models, the developed computer code represents a useful tool for flight dynamic analysis and control design for a fixed-wing aircraft.…”
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Thesis -
27
Experimental investigation of the vortical flow around a reverse delta wing using PIV
Published 2010“…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 a plane perpendicular to the free stream direction and their dependence on angles of attack and roll angles at chord based Reynolds number.…”
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Proceeding Paper -
28
Prediction of energy absorption capability of curved panel structure; for wing leading edge study
Published 2012“…This paper works on the curvature effect of wing leading edge structure subjected to impact loading. …”
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Article -
29
Experimental study of impact on carbon-fiber-epoxy composite wing leading edge structure
Published 2014“…This paper works on the curvature composite structure for wing leading edge application using fabric carbon/epoxy material subjected to impact loading. …”
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Article -
30
Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow
Published 2016“…In this paper attention is focussed on study of effect of Aspect ratio of the wing on roll moment derivatives at various angle of attack and Mach number for a Supersonic flow. …”
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Article -
31
The Fixed wing UAV usage on land use mapping for gazetted royal land in Malaysia
Published 2020“…The study deals with the usage of fixed wing unmanned aerial vehicle (UAV) in verifying boundary for gazetted royal land, which the other sight of efficacy of UAV has been tested in area of urban planning. …”
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Proceeding Paper -
32
Impact of a reverse delta type add-on device on the flap-tip vortex of a wing
Published 2016“…The effect of interactions of vortices produced by an outboard flap-tip of a half-span wing (NACA 23012 in landing configuration) and a slender reverse delta type add-on device, placed in the proximity of the outboard flap-tip, on the upper surface of the half-span wing is investigated using Particle Image Velocimetry in a closed loop low speed wind tunnel. …”
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Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges
Published 2014“…In the Present paper effect of angle of incidence on Stiffness derivative of a delta wing with Curved leading edges for attached shock case in Supersonic Flow has been studied. …”
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Article -
35
Design, fabrication and experimental testing of IIUM free wing unmanned aerial vehicle (IIUM-FWUAV)
Published 2011“…In this work, IIUM’s first free wing unmanned aerial vehicle model (IIUM-FWUAV) was designed, fabricated, tested and investigated experimentally. …”
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Article -
36
Pitch and roll derivatives of a delta wing with curved leading edge in high speed flow
Published 1990“…Ghosh's unified similitude has been applied to oscillating delta wings of arbitrary plan forms in supersonic/ hyper- sonic flow. …”
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Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge
Published 2015“…In the Present paper effect of angle of incidence on Damping derivative of a delta wing with Curved leading edges (for a full sine wave) for attached shock case in Supersonic Flow has been studied. …”
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Article -
39
Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)
Published 2011“…Integration of the streamwise vorticity shows a mild outboard wing loading shift for outboard loading case 1, while the outboard loading case 2 leads to a reduction in the span-wise circulation with no change in the spanwise load distribution. …”
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Article -
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Avrupa ve ABD'de Sağcı Popülizm ve Din (Right-wing populism and religion in Europe and the USA)
Published 2022“…This article aims to examine the rise and political influence of right-wing populism in Western Europe, Central Europe and the USA after 9/11. …”
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