Showing 21 - 40 results of 4,834 for search '((spinal OR like) OR ((((cheng OR thin) OR pin) OR (sping OR wing)) OR peng))', query time: 0.24s Refine Results
  1. 21

    Wearable bio-adhesive metal detector array (BioMDA) for spinal implants

    Published 2025
    “…Dynamic tracking of spinal instrumentation could facilitate real-time evaluation of hardware integrity and in so doing alert patients/clinicians of potential failure(s). …”
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    Article
  2. 22

    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)
  3. 23
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    Dielectric dynamics of epitaxial BiFeO3 thin films by Ren, Peng, Liu, Peng, Xia, Bin, Zou, Xi, You, Lu, Wang, Junling, Wang, Lan

    Published 2013
    “…We report the detailed study on the low temperature dielectric dynamics of the epitaxial BiFeO3 thin films grown on Nb-doped SrTiO3 substrate. The results indicate that the contributions from the thin film dominate the dielectric response, although it comes from both the thin film and the electrode interface. …”
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    Journal Article
  5. 25

    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)
  6. 26

    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)
  7. 27
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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)
  9. 29

    Additive-free electrophoretic deposition of graphene quantum dots thin films by Nguyen, Tam D., Geuli, Ori, Yeo, Loo Pin, Magdassi, Shlomo, Mandler, Daniel, Tok, Alfred Iing Yoong

    Published 2021
    “…This low-cost and eco-friendly GQD thin film is a promising material for various applications, for example, transparent conductors, supercapacitors and heat conductive films in smart windows.…”
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    Journal Article
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    Is clicking mechanism good for flapping wing micro aerial vehicle? by Chin, Yao Wei, Lau, Gih Keong

    Published 2014
    “…The click mechanism system is designed like a thin elastic plate which was compressed until bent, with its center point stable at either the top most extreme or the bottom most extreme positions. …”
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    Conference Paper
  12. 32

    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
    “…Forward osmosis (FO) has gained attention for its reduced fouling propensity. Traditional FO thin-film composite membranes, akin to reverse osmosis (RO)-like FO membranes, feature a dense and tight polyamide (PA) selective layer for high solute rejection but relatively low water permeability. …”
    Article
  13. 33

    “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
  14. 34

    Case Volume Justification of 3D-Navigated Spinal Procedures: A Cost-Benefit Analysis by Suri, Ikaasa, Suri, Mehr, Hu, James, Dedhia, Siddarth K., Yaeger, Kurt

    Published 2023
    “…Abstract 3D image-guidance platforms have transformed spinal surgery by enhancing visualization, increasing precision, and improving patient outcomes. …”
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    Article
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    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)
  17. 37

    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)
  18. 38

    Aerodynamics of a wing body with different Winglet Cant Angle. by Bakhai, Mit Piyush, Mat, Shabudin, Musa, Nur Amalina

    Published 2023
    “…This paper presents the effects of winglet Cant angle on the aerodynamic characteristics of the wing. Winglet Cant Angle (WCA) is the angle between the vertical exis and the winglet. …”
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    Conference or Workshop Item
  19. 39

    Filmwise condensation of steam on sinusoidal pin fin arrays : effects of fin height and fin pitch by Ho, Jin Yao, Leong, Kai Choong, Wong, Teck Neng

    Published 2020
    “…An experimental investigation on the use of sinusoidal pin fins to enhance filmwise condensation of steam on vertical plates was carried out. …”
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    Journal Article
  20. 40

    Butterfly-like micro air vehicle by Yang, Xiaobin

    Published 2018
    “…In this report, the author would discuss the detailed design specification and fabrication process of the butterfly-like MAV. Dynamic tests were conducted on a force cell and with a high-speed camera to record the motion of flapping wing, four sets of thrust and power in different frequency would be obtained, compared, and concluded. …”
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    Final Year Project (FYP)