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441
Solution processed transition metal oxides selective contacts for Si heterojunction solar cells
Published 2021“…In this work, we have first prepared hole selective contacts using solution processed MoOx (s-MoOx) by spin-coating and physical evaporated MoOx (e-MoOx) by electron beam evaporator. …”
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Thesis-Doctor of Philosophy -
442
Investigations into femtosecond laser hybrid manufacturing for 3D power sources
Published 2021“…First, in the design phase, acceleration and deceleration ‘wings’ are added to designs to reduce the impact of uneven fluence from mechanical movement of the galvano-scanner mirrors. …”
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Thesis-Doctor of Philosophy -
443
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) -
444
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 -
445
Optimization of transition maneuvers through aerodynamic vectoring
Published 2013“…Compared to the fixed-wing aircraft case, the angle of incidence of the wing provides an additional independent control variable in the optimization problem formulation. …”
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Journal Article -
446
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) -
447
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) -
448
To determine the effect of peening on residual stresses
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Research Report -
449
PAS : balancing inclusion and tradition
Published 2011“…The Islamic Party of Malaysia is reaching out to non-Muslim voters by forming a new wing of non- Muslim supporters, promoting good governance and playing down the Islamic state. …”
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Commentary -
450
Fluid to composite structure interaction
Published 2011“…Fabrication of the mount and the wing was done and initial designs were drawn out using the Solidworks program. …”
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Final Year Project (FYP) -
451
Deciphering the Role of a Coleopteran Steering Muscle via Free Flight Stimulation
Published 2016“…We investigated the role of a muscle involved in wing articulation during flight in a coleopteran. …”
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Journal Article -
452
When Islamists play by the rules yet change the game
Published 2011“…The recent upgrading of the PAS Supporters Club to a legal entity, complete with party constitution amendments that recognize the new wing, not only makes the PAS promise of “PAS for all” selffulfilling, it provides the party an opportunity to lead the change away from race-based politicking.…”
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Commentary -
453
Nonlinear modelling and control of a quadplane
Published 2018“…Vertical Take-off and Landing (VTOL) capabilities of fixed-wing UAV is currently being researched because of its ability to takeoff/land like rotor-craft, yet transition to forward flight like a fixed-wing. …”
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Thesis -
454
Immobilization of cyclodextrin glucanotransferase on electrospun polyvinyl alcohol nanofibers
Published 2014“…In this study, cyclodextrin glucanotransferase (CGTase) enzyme was successfully immobilised on PVA nanofibers via post-spinning and simultaneous electrospraying and electrospinning. …”
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Thesis -
455
Design and test of synthetic jet actuator for small UAVS
Published 2012“…Besides flow visualization demonstrates actuators’ capability to suppress flow separation on LS (1)-0421 wing model. This lays the foundation for its potential application on unmanned aerial vehicle.…”
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Final Year Project (FYP) -
456
Labour pains: mothers and motherhood on the British left in the twentieth century
Published 2025“…British left-wing politics does not know what to think about mothers. …”
Journal article -
457
Development of a multi-rotor UAV : structural material & key component analysis
Published 2018“…For instance, such areas include the undercarriage and the internal structure of the wing, where they are constantly subjected to surface and body forces. …”
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Final Year Project (FYP) -
458
Global borders : power, fragility, and ‘a kind of fiction’ (Editorial introduction)
Published 2021“…With the gentlest wafting of pollen from a summer breeze or a bee’s wing, the fixed categories borders inscribe can blossom into hybridities.…”
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Journal Article -
459
Development of solar power systems for solar UAV : evaluation of nomura MPPTs at sub-zero temperatures & solar modules encapsulation
Published 2014“…In addition, the energy generated by the solar cells at the time of Flight Test at India, Kanpur was calculated to check if the number of solar cells to be placed on the wing is sufficient. The deliverables for this project include a prototyped wing laden with 6 solar modules with the dimensions of 3.2 metres by 1.26 metres. …”
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Final Year Project (FYP) -
460
Grating network of ZnO nanostructure
Published 2011“…Through a vapor-phase transport method, a three-dimensional network nanostructure of ZnO, which is similar to the microstructures of a butterfly wing, was fabricated by using zinc powders as the source. …”
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Journal Article