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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) -
23
Fiksyen PASCAKOLONIAL : YANG MENJAJAH DAN DIJAJAH /
Published 2010“…Kesusasteraan pascakolonial merupakan suatu bidang kesusasteraan yang masih baharu kerana istilah pascakolonial itu hanya tercatat dalam Oxford English Dictionary yang terbit pada tahun 1959, iaitu selepas kebanyakan negara Barat mencapai kemerdekaannya. …”
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Rabiatul Adawiyah : SRIKANDI YANG AGUNG PENGABDIANNYA /
Published 2024“…Khabar betapa bayi yang bakal dilahirkan, suci dna terhormat oleh baginda sendiri dalam mimpi ayahnya. …”
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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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Citra Wanita yang Memancarkan Nilai Murni dalam Novel Popular yang Diadaptasi daripada Novel Bersiri (S/O: 13234)
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Monograph -
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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) -
29
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) -
30
Investigation and fabrication of tiltrotors/tiltwings with morphing wing mechanisms
Published 2011Get full text
Final Year Project (FYP) -
31
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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Supersymmetric Yang-Mills, spherical branes, and precision holography
Published 2020“…Using supersymmetric localization we compute the free energy and BPS Wilson loop vacuum expectation values for planar maximally supersymmetric Yang-Mills theory on Sd in the strong coupling limit for 2 ≤ d < 6. …”
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Supersymmetric Yang-Mills, spherical branes, and precision holography
Published 2019“…Using supersymmetric localization we compute the free energy and BPS Wilson loop vacuum expectation values for planar maximally supersymmetric Yang-Mills theory on Sd in the strong coupling limit for 2≤d<6. …”
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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) -
38
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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“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 -
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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)