Missing links in The China Model by Li, Chenyang

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Unit-linked policies in Singapore by Ong, Yee Chen, Poh, Chee Chung

“…In recent years, unit-linked products have gained popularity in the life industry. …”
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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

“…The theory for flapping wing aerodynamics is that, by increasing the angle of attack of the wing, the wing is able to achieve an increasing lift coefficient and in turn a larger lift force until a maximum is reached. …”
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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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Dwarf kingfisher-inspired bionic flapping wing and its aerodynamic performance at lowest flight speed by Mohd Firdaus Bin Abas, Singh, Balbir, Kamarul Arifin Ahmad, Ng, Eddie Yin Kwee, Khan, Tabrej, Sebaey, Tamer A.

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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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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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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

“…Membrane technologists have therefore diversified their focus into non-RO-like FO technologies, particularly membranes resembling nanofiltration (NF)-like FO and ultrafiltration (UF)-like FO selective layers. …”

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

“…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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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

“…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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Butterfly-like micro air vehicle by Yang, Xiaobin

“…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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Minimal type inference for Linked Data consumers by Ciobanu, Gabriel, Horne, Ross, Sassone, Vladimiro

Subjects: “…Linked Data…”
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Learning to Ask Like a Physician by Lehman, Eric(Computer scientist)

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Drag reduction in fish-like locomotion by Barrett, D.S., Triantafyllou, M.S., Yue, D.K.P., Grosenbaugh, M.A., Wolfgang, M.J.

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