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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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42
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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43
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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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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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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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 -
47
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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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 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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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 differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)
Published 2011“…Result of the outboard loading case 2 shows a limited effect in terms of the wing tip vortex structure. This can be due to the relatively large separation distance between the wing tip and the deployed spoilers, preventing the spoiler wake/wing tip vortex interaction in the near field.…”
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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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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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Enhancing Mechanical Characteristics of 6061-T6 with 5083-H111 Aluminum Alloy Dissimilar Weldments: A New Pin Tool Design for Friction Stir Welding (FSW)
Published 2024“…The experiment involved the welding of dissimilar aluminum alloys (AA5086-H111 to AA6061-T6) using a novel pin tool design with welding parameters such as holding time, pin tool length, tool spindle speed, and linear speed fine-tuned through a design of experiment (DOE) approach. …”
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The English wing spinet of the 17th and 18th centuries: with special reference to the extant Haward spinets indtroducing newly discovered evidence for Samuel Pepys' Haward spinet and Queen Anne's Haward spinet
Published 2021“…The wing spinet, evidently introduced to England in 1663 by its acknowledged inventor, Gerolamo Zenti, displaced the virginal in the 1680s and was, in turn, displaced by the square piano a century later. …”
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Thesis -
60
Feedback controller and observer design to maximize stability radius
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Proceeding Paper