Showing 21 - 40 results of 910 for search '(((spinal OR shinae) OR (pine OR spine)) OR ((spinn OR (ping OR wing)) OR pin))', query time: 0.25s Refine Results
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    Ethnoichthyology of the First Record of Spine Bahaba (Bahaba polykladiskos) from Muar, Johor, Malaysia by Ilham-Norhakim, Mohd Lokman, Mohd Faudzir, Najmuddin, Hidayah, Haris, Othman, Nursyuhada, Ramli, Ramli, Sariyati Nur Hartini, Sariyati Nur Hartini, Rasul Abdullah, Halim Muhammad, Abdullah-Fauzi, Abdullah-Fauzi, Akmal, Fawwazah, Abdul-Latiff, Muhammad Abu Bakar

    Published 2024
    “…The Spine Bahaba (Bahaba polykladiskos), locally known as 'Gelama Tirusan,' is a member of the Sciaenidae fish family that is distributed across Southeast Asia, reaching as far as North Australia. …”
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    Article
  3. 23

    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
  4. 24

    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)
  5. 25

    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)
  6. 26

    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)
  7. 27

    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
  8. 28

    Somatosensory and clinical profiles of patients with spine-related and clinical framework-based neck–arm pain by Kapitza, C, Ballenberger, N, Luedtke, K, Schmid, AB, Tampin, B

    Published 2025
    “…A recently developed mechanism-based clinical framework for spine-related pain distinguishes between spinally referred pain without neurological deficits (somatic referred pain, heightened nerve mechanosensitivity, radicular pain), with neurological deficits (radiculopathy), and mixed-pain presentations. …”
    Journal article
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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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    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
  17. 37

    “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

    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)
  19. 39

    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)
  20. 40

    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