An investigation of finite wings with leading edge protuberances by Gan, Christopher De Hao

“…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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Multiple LOD-FDTD method for inhomogeneous coupled transmission lines and stability analyses by Heh, Ding Yu, Tan, Eng Leong

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Filmwise condensation of steam on pin fin arrays fabricated by selective laser melting by Ho, Jin Yao, Leong, Kai Choong

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An experimental investigation on finite wings with leading-edge protuberances by Teo, Marcus Jun Jie

“…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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An experimental investigation of vibration testing of aircraft wing structure by Chew, Chor Loon.

“…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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Investigation and fabrication of tiltrotors/tiltwings with morphing wing mechanisms by Hon, Shah Kiat.

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Investigation of the effects of wing membrane slackness on thrust generation by Chua, Jasper Dong Qiu

“…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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An empirical study on service quality of shipping lines and its relationship with customer satisfaction by Chye, Hui Hong, Lim, Imy, Soh, Hui Ping

“…The study uses shipping lines in Singapore as the primary setting. It aims to gain insight on the criteria used by shippers in the evaluation of service quality of shipping lines, as well as explores the underlying relationship between service quality and customer satisfaction. …”
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Design of pinned and rigid bolted connections using BS 5950:2000 and Eurocode 3 by Xie, Yunshen.

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Compact true time delay line with partially shielded coplanar waveguide transmission lines by Lim, Hong Yi, Ng, Geok Ing, Leong, Yoke Choy

“…This paper presents a method to attain a compact true time delay line with a partially shielded coplanar waveguide transmission line. …”
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Mining on-line user reviews by Bin, Shi

“…In this report, we propose a system for mining on-line user product reviews. Each sentence in a review is analyzed to extract the user’s opinion / orientation of a product feature. …”
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Transmission line with gaseous cavitation by Chen, Junting.

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Behaviour of joints in tunnel linings by Alevey, Niall Mac, Ashraf Mohamed Hefny

“…Precast concrete tunnel segments are used extensively to construct tunnel linings. In order to reduce bending moments the lining must be flexible. …”
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Crossing the line : harassed on the web by Thor, Venessa Xing Ying, Yee, Wendy Shu Yan

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Gaseous cavitation in transmission line by Yeo, Wei Jian

“…A comprehensive study on gaseous cavitation in transmission lines will be presented. A model will be developed to simulate and forecast the effect of cavitation. …”
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Press freedom : drawing the line by Santos, Vergel O.

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“Clicking” compliant mechanism for flapping-wing micro aerial vehicle by Chin, Yao-Wei, Lau, Gih Keong

“…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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Design and characterisation of bio-inspired thorax for flapping-wing robotfly by Teo, Wei Xiong.

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

“…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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Is clicking mechanism good for flapping wing micro aerial vehicle? by Chin, Yao Wei, Lau, Gih Keong

“…It also showed quick wing reversal and is able to produce consistent large wing stroke (~115°). …”
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