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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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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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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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Bag of remembrance: a cultural biography of red-white-blue, from Hong Kong to Louis Vuitton
Published 2018Get full text
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