Showing 1 - 20 results of 838 for search '((((wing OR shing) OR spink) OR (swingge OR ssspingge)) OR ((sslingggna OR sspingna) OR ming))', query time: 0.19s Refine Results
  1. 1

    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)
  2. 2

    Investigation of wing rock on delta wing part 2 : dynamic characteristics by Wong, Charles Junxin.

    Published 2009
    “…This final year project focuses on the study of wing rock for delta wings at high angles of attack in a water tunnel. …”
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    Final Year Project (FYP)
  3. 3

    Insect inspired two-wing flapping wing micro air vehicle by Ma, Jiacheng

    Published 2012
    “…This report presents an in-depth study of the flight of the hawk moth Manduca Sexta, with the goal of replicating its wing motion for the design of a Micro Air Vehicle. …”
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    Final Year Project (FYP)
  4. 4

    Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis by Gan, Calvin Cheng Rui

    Published 2009
    “…This final year project focuses on the study of wing rock of delta wings at high angles of attack in a water tunnel. …”
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    Final Year Project (FYP)
  5. 5

    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)
  6. 6

    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)
  7. 7

    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)
  8. 8

    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)
  9. 9

    Unravelling the complex meanings and origins of zisha teapots in the Ming and Qing dynasties by Gao, X

    Published 2023
    “…The unglazed teapots, made from <em>zisha</em> clay using a slabbuilding technique, have been appreciated by tea consumers since the Late Ming dynasty onwards. The study employs a multidisciplinary approach, including ethnographic research, archaeological science, historical analysis, the concept of <em>chaîne opératoire</em>, and experimental archaeology, to examine various data sources and gain a comprehensive understanding of the origins and development of <em>zisha</em> teapots.…”
    Thesis
  10. 10
  11. 11

    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)
  12. 12

    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)
  13. 13

    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)
  14. 14

    Maternal neonaticide, shame and social melancholy in Hsu-Ming Teo's Love and Vertigo by Zhou, Qiaoqiao, Omar, Noritah

    Published 2023
    “…Most critics read Love and Vertigo (2000) by Chinese-Australian writer Hsu-Ming Teo as a novel about diaspora and migrancy. …”
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    Article
  15. 15

    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)
  16. 16

    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)
  17. 17
  18. 18

    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)
  19. 19

    “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
  20. 20

    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)