Showing 21 - 40 results of 484 for search '((spinna OR wing) OR ((((aina OR ainaa) OR (aina OR ainaa)) OR (swing OR (pina OR swing))) OR pin))', query time: 0.21s Refine Results
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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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    “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
  10. 30

    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)
  11. 31

    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)
  12. 32

    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
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    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
  14. 34

    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
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