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spink » spin (Expand Search), spine (Expand Search), spins (Expand Search)
ping » ling (Expand Search), ming (Expand Search), peng (Expand Search)
wing » owing (Expand Search), wang (Expand Search), wong (Expand Search)
spinae » spine (Expand Search), shinae (Expand Search), spina (Expand Search), sainae (Expand Search), sninae (Expand Search)
shing » ching (Expand Search), sheng (Expand Search), shin (Expand Search)
spinal » spinl (Expand Search), sainal (Expand Search), sninal (Expand Search)
pina » pin (Expand Search), aina (Expand Search), nina (Expand Search)
bina » bin (Expand Search), bing (Expand Search)
spink » spin (Expand Search), spine (Expand Search), spins (Expand Search)
ping » ling (Expand Search), ming (Expand Search), peng (Expand Search)
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Wearable bio-adhesive metal detector array (BioMDA) for spinal implants
Published 2025“…The customized decoupling models developed facilitate the precise determination of the horizontal and vertical positions of the implants with incredible levels of accuracy (e.g., <0.5 mm). These data support the potential use of BioMDA in real-time/dynamic postoperative monitoring of spinal implants.…”
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Article -
22
Investigation and fabrication of tiltrotors/tiltwings with morphing wing mechanisms
Published 2011“…This report included a historical study of tiltrotor/tiltwing developments and reviewed current developments in morphing aircrafts and V/STOL aircrafts. In order to provide a platform for researches and test-bedding of different technologies, a prototype was designed with low cost and ease of manufacturing in mind. …”
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Final Year Project (FYP) -
23
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 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) -
26
5G : The 5th Generation Mobile Networks /
Published 2024Subjects: “…5G mobile communication systems…”
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software, multimedia -
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Vehicular localization using 5G V2X
Published 2022“…This project will discuss on different vehicle positioning methods related to the 5G V2X. Besides, a simulation solution using mmWave signals to complete vehicle positioning will be given. …”
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Final Year Project (FYP) -
29
Case Volume Justification of 3D-Navigated Spinal Procedures: A Cost-Benefit Analysis
Published 2023“…Abstract 3D image-guidance platforms have transformed spinal surgery by enhancing visualization, increasing precision, and improving patient outcomes. …”
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Article -
30
AB078. Patterns of treatment delay in patients with symptomatic metastatic epidural spinal cord compression
Published 2024Subjects: Get full text
Journal Article -
31
“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 -
32
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) -
33
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) -
34
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 -
35
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 -
36
Electron-donating five-membered heterocyclic modulated electronic states boosting visible-light-driven H2O2 production
Published 2024Subjects: Get full text
Journal Article -
37
A study on the career choices of tax professionals in the big five CPA firms in Singapore.
Published 2008“…This project is a study on the career choices of tax professionals in the Big Five CPA firms in Singapore. The project explores the reasons why they choose to join, stay or leave the tax profession.…”
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Final Year Project (FYP) -
38
Infection risk of SARS-CoV-2 in a dining setting : deposited droplets and aerosols
Published 2022“…The AER from speaking was 24698 #/min in the size range of 0.3-5.5 μm, while the DDR was 365 #/min in the size range of 43-2847 μm. …”
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Journal Article -
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