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Solar UAV : design and fabrication of structural test rig for loading and testing a 7.5m half wing
Published 2013“…The objective of the project was to design and manufacture a Solar UAV with wingspan of 17.5m, take-off weight of 60kg and having an endurance of 24 hours. …”
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Final Year Project (FYP) -
4
Investigation of wing rock on delta wing part 2 : dynamic characteristics
Published 2009“…This final year project focuses on the study of wing rock for delta wings at high angles of attack in a water tunnel. …”
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Final Year Project (FYP) -
5
Insect inspired two-wing flapping wing micro air vehicle
Published 2012“…This report presents an in-depth study of the flight of the hawk moth Manduca Sexta, with the goal of replicating its wing motion for the design of a Micro Air Vehicle. …”
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Final Year Project (FYP) -
6
Reactivating and reorganizing activity-silent working memory: two distinct mechanisms underlying pinging the brain
Published 2025“…Recent studies have proposed that visual information in working memory (WM) can be maintained in an activity-silent state and reactivated by task-irrelevant high-contrast visual impulses (“ping”). Although pinging the brain has become a popular tool for exploring activity-silent WM, its underlying mechanisms remain unclear. …”
Journal article -
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Enrichment of package antenna approach with dual feeds, guard ring, and fences of vias
Published 2010“…The design guideline of the guard ring and fence of vias for the package antenna approach is developed for the first time. …”
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Journal Article -
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Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis
Published 2009“…This final year project focuses on the study of wing rock of delta wings at high angles of attack in a water tunnel. …”
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Final Year Project (FYP) -
9
Computational fluid dynamics of flapping wings
Published 2013“…This paper studies the Computational Fluid Dynamics of flapping wings using the JET Code, which uses the large eddy simulation model and the immersed boundary method. …”
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Final Year Project (FYP) -
10
Adaptive wing and fuselage structure for UAVs
Published 2013“…These wonderful characteristics enable the UAVs to be contractible/deployable, warping and morphing wing. However, there are still serious short-comings with these inflated wings, including the ultra-high compressed-air pressure, difficulty in wing-profile shaping and unreliable. …”
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Final Year Project (FYP) -
11
Analysis of flapping-wing compliant mechanism
Published 2014“…Wing inertia is the mass property that defines the torque needed by flapping-wing creatures to accelerate and decelerate the wings. …”
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Final Year Project (FYP) -
12
Bi-stable mechanism for morphing wings
Published 2015“…Morphing wing aircraft has been a complicated topic that involves higher level of knowledge that would be difficult for us to grasp right off. …”
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Final Year Project (FYP) -
13
Design of differential microstrip ring antenna
Published 2021“…In this Final Year Project, the study of a differential microstrip ring antenna operating at 5.2GHz will be conducted. …”
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Final Year Project (FYP) -
14
Study on properties of fibre ring resonators
Published 2017“…Both linear and non-linear applications were tested with different coupling ratio optical coupler under continuous wave and pulsed light injection respectively. A set of five couplers with different coupling ratio will be used individually on the fibre ring resonator prototype. …”
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Final Year Project (FYP) -
15
Topological pumping in Aharonov – Bohm rings
Published 2020“…Here, we study both effects together: topological pumping of interacting particles through Aharonov–Bohm rings. This system can prepare highly entangled many-particle states, transport them via topological pumping and interfere with them, revealing a fractional flux quantum. …”
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Journal Article -
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Vertical split-ring resonators for plasmon coupling, sensing and metasurface
Published 2018Subjects: Get full text
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Conference Paper -
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Design and fabrication of piezoelectrically driven wing flapper
Published 2011“…This study focused on reproducing the flapping mechanism observed in insect flight using piezoelectric material as its driving mechanism. The result was a wing flapper capable of achieving large wing strokes and weighs 1.26gram. …”
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Final Year Project (FYP) -
18
Micro air vehicles : flapping wing propulsion
Published 2011“…The wing used was a straight wing of airfoil NACA 0012. …”
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Final Year Project (FYP) -
19
An investigation of finite wings with leading edge protuberances
Published 2017“…In the present study, Particle Image Velocimetry (PIV) was carried out in a water tunnel at a Reynolds number of 2.0 x 10^4 to investigate the cross stream flow around finite wings with leading-edge protuberances. Results obtained confirm that the protuberances lead to the generation of counter-rotating vortex pairs (CVPs), similar to the function of vortex generators. …”
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Final Year Project (FYP) -
20
A study of five derivatives markets in the Asia-Pacific Basin
Published 2014Get full text
Final Year Project (FYP)