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441
Soft actuators and their fabrication for bio-inspired mobile robots
Published 2016“…Dielectric elastomer actuators (DEA), which are capable of muscle-like actuation, have potential to drive insect-inspired flapping-wing robotfly. They have not been successfully used to drive flapping wings due to various limitations. …”
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Research Report -
442
Preliminary Investigation of 4D Printing Technology for Deployable UAV Development
Published 2016“…Current unmanned aerial vehicles (UAVs) are large in size due to fixed wings and mechanical components. 4D printing is a technology that allows shape transformation (e.g. compaction, extension) of a 3D printed object. …”
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Conference Paper -
443
Morphing structures
Published 2009“…This project aims to investigate specific applications of smart materials in the design of a morphing wing. Smart materials have great potential in many fields, and are already widely used in some fields. …”
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Final Year Project (FYP) -
444
Design and develop an ornithopter
Published 2011“…Animal in other hand has unique style; bird for example is able to flying by flapping the wings. It is very interesting way to perform flight. …”
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Final Year Project (FYP) -
445
CFD investigation of a distributed propulsion system
Published 2022“…Numerical simulation using computational fluid dynamics is used in this paper to determine the lift and drag forces, and subsequently the aerodynamic efficiency of a 3-D finite wing in ANSYS Fluent. The computational domain utilized an overset mesh with the component consisting of the finite wing and equally spaced momentum sources representing propellers mounted on the wing. …”
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Final Year Project (FYP) -
446
Design and development of composite structure for a micro-UAV
Published 2012“…This report describes the design process and fabrication of a composite fuselage for a 2kg class micro-UAV which is propelled by flapping wings. It begins with the comparison and selection of fabrication process. …”
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Final Year Project (FYP) -
447
Optimization of transition maneuvers through aerodynamic vectoring
Published 2013“…This paper discusses the optimization of transition maneuvers between hover and cruise for small aircraft using a novel aerodynamic vectoring feature, which is achieved by allowing the wing to have variable incidence angle with respect to the fuselage. …”
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Journal Article -
448
Cell charactetization in differnet regions of the native annulus fibrous in a porcine intervetebral disc model through cell sorting and molecular analysis
Published 2016“…The factors that lead to low back pain are complex, there has been more evidence that shows that intervertebral disc degeneration serves as a major contributor leading to the destabilization of the spinal motion segment hence resulting in pain and disability. …”
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Final Year Project (FYP) -
449
Butterfly-like micro air vehicle
Published 2018“…Butterfly cannot hover, but it has unique aerodynamic characteristics such as undulating body motion and low wing loading. Development of flapping wing micro air vehicle is mainly focus on the hovering birds and inserts. …”
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Final Year Project (FYP) -
450
Dragonfly (Sympetrum flaveolum) flight : kinematic measurement and modelling
Published 2013“…Such arrangement also eases the difficulties in rotating the wing during pronation by bending the leading edge forward and flattening the wing. …”
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Journal Article -
451
A Self-Polymerizing Mesh of Nano-Tethers for the Mechanical Constraint of Degraded Intervertebral Discs—A Review of 25 Years of Pre-Clinical and Early Clinical Research
Published 2024“…It is intended that this review of a novel nano-scale material-based solution for mechanical deficiencies in biologically limited tissues may provide a helpful example for other innovations in spinal diseases and similarly challenging musculoskeletal disorders.…”
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Article -
452
Design and investigation of air-cooled heat sinks using 3D printing technology
Published 2016“…This study presents the heat transfer performance of five pin fin heat sinks that have been fabricated using Selective Laser Melting. …”
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Final Year Project (FYP) -
453
Design of wideband low-loss reconfigurable reflectarray antenna
Published 2024“…It proposes an RRA design that integrates a PIN diode with air gap. The switch of the reconfigurable unit is directly mounted on the reflective element, reducing the loss introduced by the switching device. …”
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Thesis-Master by Coursework -
454
Effect of adding global postural re-education to Kendall exercises for treating asymptomatic forward head posture: a single-blinded randomized controlled trial
Published 2025“…Conclusions: The added effect GPR technique to Kendall exercises significantly improved CVA, CROM, NDI, chest expansion, and spinal mobility in subjects with FHP.…”
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Article -
455
3D spine shape estimation from single 2D DXA
Published 2024“…Consequently, extracting the spinal geometry in 3D would help quantify these spinal deformations and aid diagnosis. …”
Conference item -
456
A 1-bit 16×16 reconfigurable intelligent surfaces array for C-band
Published 2025“…RIS array is achieved by combining a number of basic elements together with PIN diodes which control the on and off state of RIS units. …”
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Thesis-Master by Coursework -
457
A numerical study on bio-inspired aerofoils oscillating in tandem
Published 2018“…As a dragonfly has two pairs of wings, a natural progression would be to expand on these findings into investigating the effects and flow interactions between two tandemly-positioned aerofoils in synchronised pitching motion. …”
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Final Year Project (FYP) -
458
Komet
Published 2015“…Snow falls, star falls One step, one beginning Two worlds meet one A trail to ever last Butterfly city, never night city Red light, green light Ghosts of thousand faces Beckoning from the wall Good, bad, and ugly Stone ocean, iron sky Omens of million wings The lady fortune frowns So ends the pendulum Farewell goodbye An empty longing For things long gone -In memory of all good things-…”
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Final Year Project (FYP) -
459
Design of a pneumatic launcher and glider
Published 2009“…The size of this glider is about 150mm for the wing span and 200mm for the fuselage. The whole system of this design was based on the pneumatic power and the aerodynamics of a fixed wing. …”
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Final Year Project (FYP) -
460
Fracturing Processes in Specimens with Internal vs. Throughgoing Flaws: An Experimental Study Using 3D Printed Materials
Published 2024“…This investigation showed that wing cracks appeared in specimens with throughgoing flaws, while wing cracks with petal cracks were associated with the internal flaws. …”
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Article