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spinal » sspinal (Expand Search)
pin » spin (Expand Search)
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pings » spings (Expand Search), rings (Expand Search), pins (Expand Search), pigs (Expand Search), lings (Expand Search), mings (Expand Search), pengs (Expand Search)
ping » sping (Expand Search), ling (Expand Search), ming (Expand Search), peng (Expand Search)
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Objects of Collaboration: Roles and Sequences of Objects in Spanning Knowledge Group Boundaries in Design
Published 2024“…<jats:title>Abstract</jats:title> <jats:p>Spanning knowledge group boundaries is both a source of and barrier to design performance and innovation. …”
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Article -
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Objects of Collaboration: Roles of Objects in Spanning Knowledge Boundaries in a Design Company
Published 2024“…These findings are significant because they clarify the roles of objects in cross-boundary design work and suggest ways for designers to more effectively use objects to span knowledge boundaries.</jats:p>…”
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Article -
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Domain wall pinning through nanoscale interfacial Dzyaloshinskii-Moriya interaction
Published 2022“…We have also studied pinning in a device with five successive pinning sites. …”
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Journal Article -
25
Comparative analysis of dehydration techniques on phytochemical and antibacterial properties on pink and purple flowers impatiens walleriana
Published 2025“…Microwave-dried leaf extracts were evaluated for antibacterial activity using the disc diffusion method. Both pink and purple flower varieties demonstrated inhibition of Gram-positive and Gram-negative bacteria, with the pink flower showing greater antibacterial effects. …”
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Conference or Workshop Item -
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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) -
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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) -
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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) -
29
Wearable bio-adhesive metal detector array (BioMDA) for spinal implants
Published 2025“…Dynamic tracking of spinal instrumentation could facilitate real-time evaluation of hardware integrity and in so doing alert patients/clinicians of potential failure(s). …”
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Article -
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Filmwise condensation of steam on pin fin arrays fabricated by selective laser melting
Published 2020Subjects: Get full text
Journal Article -
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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) -
32
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) -
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Investigation and fabrication of tiltrotors/tiltwings with morphing wing mechanisms
Published 2011Get full text
Final Year Project (FYP) -
34
Investigation of the effects of wing membrane slackness on thrust generation
Published 2016“…The theory for flapping wing aerodynamics is that, by increasing the angle of attack of the wing, the wing is able to achieve an increasing lift coefficient and in turn a larger lift force until a maximum is reached. …”
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Final Year Project (FYP) -
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Design of pinned and rigid bolted connections using BS 5950:2000 and Eurocode 3
Published 2011Get full text
Final Year Project (FYP) -
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Dwarf kingfisher-inspired bionic flapping wing and its aerodynamic performance at lowest flight speed
Published 2023Subjects: Get full text
Journal Article -
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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 -
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AB078. Patterns of treatment delay in patients with symptomatic metastatic epidural spinal cord compression
Published 2024Subjects: Get full text
Journal Article -
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“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