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861
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) -
862
Wind tunnel testing of a ducted-fan unmanned aerial vehicle
Published 2011“…The experiment was then further extended to varying pitching and wing incidence angles together. Wing incidence angles were varied at different duct angles to understand the effects of interference between the two. …”
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Final Year Project (FYP) -
863
Development of morphing UAV actuated with shape memory alloy
Published 2014“…For this project, a sweeping wing mechanism actuated by Shape Memory alloys (SMAs) is designed and developed. …”
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Final Year Project (FYP) -
864
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865
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 -
866
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 -
867
Natural avian inspired ornithopter UAV
Published 2019“…Several prototypes and modular parts such as gear boxes and wings are explored to obtain varying results to obtain optimum flight worthy prototype.…”
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Final Year Project (FYP) -
868
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 -
869
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) -
870
Preliminary Investigation of 4D Printing Technology for Deployable UAV Development
Published 2016“…Additionally, the folding sequence of different parts of the wing is programmable as well by using multiple materials. …”
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Conference Paper -
871
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) -
872
To determine the effect of peening on residual stresses
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Research Report -
873
Exploring the stability and dynamics of nanobubbles
Published 2017“…These nanobubbles appear not to be stabilised by the line pinning or oversaturation that sustain surface nanobubbles. …”
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Thesis -
874
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 -
875
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) -
876
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 -
877
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 -
878
Effect of dopant solubility and excess doping on the superconducting properties of doped Nb3Sn prepared by field assisted sintering technique
Published 2024“…The Y<sub>2</sub>O<sub>3</sub> particles was also considered as a possible cause of pinning down of grain boundaries in addition to NbO leading to grain refinement through Zener pinning. …”
Journal article -
879
Morphing structures
Published 2009“…This report will focus on application of smart materials, namely Smart Memory Polymer (SMP) and Smart Memory Alloy (SMA) in the area of morphing wings. In this report, there will be four distinct designs that make use of smart materials in different ways to create geometric changes to a wing. …”
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Final Year Project (FYP) -
880
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)