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pink » link (Expand Search), ping (Expand Search), pick (Expand Search), pingk (Expand Search), spink (Expand Search)
qingge » qiangge (Expand Search), jingge (Expand Search), xingge (Expand Search)
spie » spin (Expand Search)
wing » owing (Expand Search), wang (Expand Search), wong (Expand Search)
pinna » pina (Expand Search), pinn (Expand Search), pingna (Expand Search), spinna (Expand Search)
pin » ping (Expand Search), spin (Expand Search)
pink » link (Expand Search), ping (Expand Search), pick (Expand Search), pingk (Expand Search), spink (Expand Search)
qingge » qiangge (Expand Search), jingge (Expand Search), xingge (Expand Search)
spie » spin (Expand Search)
wing » owing (Expand Search), wang (Expand Search), wong (Expand Search)
pinna » pina (Expand Search), pinn (Expand Search), pingna (Expand Search), spinna (Expand Search)
pin » ping (Expand Search), spin (Expand Search)
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21
An experimental investigation of vibration testing of aircraft wing structure
Published 2010“…This report presents the experimental investigation and vibration analysis of an aircraft wing structure using impact testing. The importance of obtaining its vibration characteristics such as the natural frequencies and mode shapes of the aircraft wing structure to prevent flutter phenomena that can eventually lead to structural failure is also reviewed. …”
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Final Year Project (FYP) -
22
Investigation and fabrication of tiltrotors/tiltwings with morphing wing mechanisms
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Final Year Project (FYP) -
23
Investigation of the effects of wing membrane slackness on thrust generation
Published 2016“…In one recent study, it was found that bats have tiny muscles within their wing membranes which allow them to change the slackness of their wing membranes during flight. …”
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Final Year Project (FYP) -
24
Design of pinned and rigid bolted connections using BS 5950:2000 and Eurocode 3
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Final Year Project (FYP) -
25
Is clicking mechanism good for flapping wing micro aerial vehicle?
Published 2014“…It also showed quick wing reversal and is able to produce consistent large wing stroke (~115°). …”
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Conference Paper -
26
“Clicking” compliant mechanism for flapping-wing micro aerial vehicle
Published 2013“…This paper presented a click mechanism, which is inspired by a Dipteran insect, for use in flapping-wing micro aerial vehicle. The clicking mechanism is integrated in a thorax-like compliant mechanism, which buckles and consequently produces a large wing stroke when driven by an electric motor. …”
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Conference Paper -
27
Design and characterisation of bio-inspired thorax for flapping-wing robotfly
Published 2010“…The design parameters were varied in the experiments and the design rules for the wing flapper are identified. These design rules lead to the first flapping wing robotfly prototype since the inception of the wing flapper research. …”
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Final Year Project (FYP) -
28
Development of control system for flapping wing micro air vehicles
Published 2017“…This report presents the understanding, design and fabrication of a simple control system for a Flapping Wing Micro Aerial Vehicle (FWMAV) to change its angle of flight. …”
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Final Year Project (FYP) -
29
Aerodynamics of a wing body with different Winglet Cant Angle.
Published 2023“…This paper presents the effects of winglet Cant angle on the aerodynamic characteristics of the wing. Winglet Cant Angle (WCA) is the angle between the vertical exis and the winglet. …”
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Conference or Workshop Item -
30
Filmwise condensation of steam on sinusoidal pin fin arrays : effects of fin height and fin pitch
Published 2020“…An experimental investigation on the use of sinusoidal pin fins to enhance filmwise condensation of steam on vertical plates was carried out. …”
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Journal Article -
31
Performance and flight dynamics characteristics of a variable sweep wing aircraft
Published 2009“…The parameters of the wings that are altered across these different morphing stages are wing root chord, tip chord and aspect ratio. …”
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Final Year Project (FYP) -
32
Determination of operating point for a propulsive wing UAV using CFD
Published 2018“…This report seeks to determine the operating point of a 2D propulsive wing UAV using CFD. CFD simulations were performed using a 2D RANS k-ε turbulence model and the rotating flow was captured using the moving reference frame method. …”
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Final Year Project (FYP) -
33
Thermal stability of trypsin inhibitor activity in winged bean (Psophocarpus tetragonolobus)
Published 1982“…The thermal stability of trypsin inhibitor activity (TIA) in six varieties of winged beans was investigated. The TIA in winged bean meals was extremely resistant to dry heat treatment. …”
Article -
34
Synaptic element for neuromorphic computing using a magnetic domain wall device with synthetic pinning sites
Published 2020“…The control of the domain wall motion with the synthetic pinning sites is demonstrated to be a reliable technique for neuromorphic applications.…”
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Journal Article -
35
The natively disordered loop of Bcl-2 undergoes phosphorylation-dependent conformational change and interacts with Pin1
Published 2013“…Finally, we show that the phosphorylated peptides of the Bcl-2 loop can bind Pin1, further substantiating the phosphorylation-mediated conformation change of Bcl-2.…”
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Journal Article -
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Simulation of suppression of vortex breakdown over delta wings by vortex filament method
Published 2008“…The purpose of perturbing the vortex core is to delay or suppress vortex breakdown over delta wings.…”
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Thesis -
39
Whose right, whose left? Analyzing the complexities of right-wing politics in Venezuela
Published 2024“…As authoritarianism and repression have increased and Venezuela’s socioeconomic decline has worsened, right-wing movements and factions have prioritized competitiveness through a centrist approach over an emphasis on ideological purity.…”
Book section -
40
Mechanism of charge transfer and its impacts on Fermi-level pinning for gas molecules adsorbed on monolayer WS2
Published 2015“…The phenomenon of Fermi-level pinning was discussed in light of the traditional and orbital mixing charge transfer theories. …”
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Journal Article