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pinna » pina (Expand Search), pinn (Expand Search), pingna (Expand Search), spinna (Expand Search)
pinnu » pinnau (Expand Search), pintu (Expand Search), pinn (Expand Search), pingnu (Expand Search), spinnu (Expand Search)
shinae » shine (Expand Search), shina (Expand Search), shinde (Expand Search)
pingna » pinggna (Expand Search), spingna (Expand Search)
pin » ping (Expand Search), spin (Expand Search)
swing » owing (Expand Search), shing (Expand Search), sowing (Expand Search), swang (Expand Search), swong (Expand Search)
wing » owing (Expand Search), wang (Expand Search), wong (Expand Search)
link » line (Expand Search)
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The design of a rail-to-rail output swing using a nested-current-mirror single-stage amplifier with a high PSRR
Published 2021“…The project is to design a Nested – Current – Mirror Operational Amplifier with Rail – to – Rail Output swing. The design is with reference to the paper written by Yan, Mak, Laws, Martins and Malobeti (2015), which consist of the basic structure of the Nested – Current – Mirror Operational Amplifier with a single output. …”
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Final Year Project (FYP) -
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An experimental investigation on finite wings with leading-edge protuberances
Published 2023“…Additionally, analysis of flows over the suction side of the wing will be conducted using Particle Image Velocimetry to determine the nature of flows over a tubercle wing against a baseline wing. …”
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Final Year Project (FYP) -
24
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) -
25
Investigation and fabrication of tiltrotors/tiltwings with morphing wing mechanisms
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Final Year Project (FYP) -
26
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) -
27
Design of pinned and rigid bolted connections using BS 5950:2000 and Eurocode 3
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Final Year Project (FYP) -
28
“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 -
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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 -
30
Current state-of-the-art of non-reverse osmosis-like forward osmosis technology
Published 2024“…Membrane technologists have therefore diversified their focus into non-RO-like FO technologies, particularly membranes resembling nanofiltration (NF)-like FO and ultrafiltration (UF)-like FO selective layers. …”
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31
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) -
32
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) -
33
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 -
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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 -
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Butterfly-like micro air vehicle
Published 2018“…In this report, the author would discuss the detailed design specification and fabrication process of the butterfly-like MAV. Dynamic tests were conducted on a force cell and with a high-speed camera to record the motion of flapping wing, four sets of thrust and power in different frequency would be obtained, compared, and concluded. …”
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Final Year Project (FYP) -
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Minimal type inference for Linked Data consumers
Published 2015Subjects: “…Linked Data…”
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Journal Article -
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