Showing 21 - 40 results of 1,888 for search '((pick OR (qingge OR qiangge)) OR (((spie OR (wing OR wong)) OR ((pinn OR ins) OR ping)) OR pin))', query time: 0.26s Refine Results
  1. 21

    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)
  2. 22

    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)
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    Domain wall pinning through nanoscale interfacial Dzyaloshinskii-Moriya interaction by Kumar, Durgesh, Chan, Jianpeng, Piramanayagam, S. N.

    Published 2022
    “…We have also studied pinning in a device with five successive pinning sites. …”
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    Journal Article
  6. 26

    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)
  7. 27

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

    Published 2011
    “…This Final Year Report (FYP) investigated the aerodynamic effects of a flapping wing. A water tunnel facility was used in the experiments, testing the effects of a wing in heaving motion on a constant, steady flow. …”
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    Final Year Project (FYP)
  8. 28

    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)
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    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)
  11. 31

    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
    “…In one recent study, it was found that bats have tiny muscles within their wing membranes which allow them to change the slackness of their wing membranes during flight. …”
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    Final Year Project (FYP)
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    Filamentous oligomer structure reconstruction and a new filament picking method for Cryo-EM micrographs by Xu, Chenrui

    Published 2022
    “…Recognizing the bottleneck step of this process, the filament picking, we developed a rapid and easy-to-use software. …”
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    Thesis-Doctor of Philosophy
  16. 36
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    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
  18. 38

    “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
  19. 39

    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)
  20. 40

    Development of control system for flapping wing micro air vehicles by Chua, Jasper Ming Song

    Published 2017
    “…This report presents the understanding, design and fabrication of a simple control system for a Flapping Wing Micro Aerial Vehicle (FWMAV) to change its angle of flight. …”
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    Final Year Project (FYP)