Showing 21 - 40 results of 4,361 for search '(((pin OR (pine OR sainae)) OR like) OR ((spinn OR (((pings OR ping) OR pins) OR wings)) OR ling))', query time: 0.27s Refine Results
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    Responses of gas exchange and growth in Merkus pine seedlings to expected climatic changes in Thailand by Koskela, Jarkko

    Published 2008
    “…Responses of gas exchange and growth in Merkus pine (Pinus merkusii Jungh. et de Vriese) seedlings to changing climate were analysed for high- and low-altitude sites in Thailand. …”
    Article
  3. 23

    Computational fluid dynamics of flapping wings by Ng, Eric Tee-Sang.

    Published 2013
    “…This paper studies the Computational Fluid Dynamics of flapping wings using the JET Code, which uses the large eddy simulation model and the immersed boundary method. …”
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    Final Year Project (FYP)
  4. 24

    Adaptive wing and fuselage structure for UAVs by Truong, Ngoc Quoc Thang.

    Published 2013
    “…These wonderful characteristics enable the UAVs to be contractible/deployable, warping and morphing wing. However, there are still serious short-comings with these inflated wings, including the ultra-high compressed-air pressure, difficulty in wing-profile shaping and unreliable. …”
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    Final Year Project (FYP)
  5. 25

    Analysis of flapping-wing compliant mechanism by Fam, Shi Jiez

    Published 2014
    “…Wing inertia is the mass property that defines the torque needed by flapping-wing creatures to accelerate and decelerate the wings. …”
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    Final Year Project (FYP)
  6. 26

    Bi-stable mechanism for morphing wings by Yang, Jingjing

    Published 2015
    “…Morphing wing aircraft has been a complicated topic that involves higher level of knowledge that would be difficult for us to grasp right off. …”
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    Final Year Project (FYP)
  7. 27

    CSS-like constructions of asymmetric quantum codes by Ezerman, Martianus Frederic, Jitman, Somphong, Ling, San, Pasechnik, Dmitrii V.

    Published 2019
    “…After establishing some theoretical foundations, best-performing CSS-like AQCs are constructed. Combining some constructions of nested pairs of classical codes and linear programming, many optimal and good pure q-ary CSS-like codes for q ∈ {2,3,4,5,7,8,9} up to reasonable lengths are found. …”
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    Journal Article
  8. 28

    Design and fabrication of piezoelectrically driven wing flapper by Xu, WeiQuan.

    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)
  9. 29

    Micro air vehicles : flapping wing propulsion by Koay, Say Seng.

    Published 2011
    “…The wing used was a straight wing of airfoil NACA 0012. …”
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    Final Year Project (FYP)
  10. 30

    An investigation of finite wings with leading edge protuberances by Gan, Christopher De Hao

    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)
  11. 31

    Walking like trees by Lim, Jonathan Yong Ern

    Published 2017
    “…Walking Like Trees was a year-long exploration of storytelling through the juxtaposition of text and image within the medium of the printed graphic novel. …”
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    Final Year Project (FYP)
  12. 32

    An experimental investigation on finite wings with leading-edge protuberances by Teo, Marcus Jun Jie

    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)
  13. 33

    An experimental investigation of vibration testing of aircraft wing structure by Chew, Chor Loon.

    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 of the effects of wing membrane slackness on thrust generation by Chua, Jasper Dong Qiu

    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)
  16. 36
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    “Clicking” compliant mechanism for flapping-wing micro aerial vehicle by Chin, Yao-Wei, Lau, Gih Keong

    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
  18. 38

    Is clicking mechanism good for flapping wing micro aerial vehicle? by Chin, Yao Wei, Lau, Gih Keong

    Published 2014
    “…It also showed quick wing reversal and is able to produce consistent large wing stroke (~115°). …”
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    Conference Paper
  19. 39

    Current state-of-the-art of non-reverse osmosis-like forward osmosis technology by Chang, Zhen Hong, Sum, Jing Yao, Lau, Woei Jye, Ang, Wei Lun, Teow, Yeit Haan, Ooi, Boon Seng, Yeap, Swee Pin

    Published 2024
    “…Membrane technologists have therefore diversified their focus into non-RO-like FO technologies, particularly membranes resembling nanofiltration (NF)-like FO and ultrafiltration (UF)-like FO selective layers. …”
    Article
  20. 40

    Design and characterisation of bio-inspired thorax for flapping-wing robotfly by Teo, Wei Xiong.

    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)