Design and fabrication of piezoelectrically driven wing flapper by Xu, WeiQuan.

“…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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Micro air vehicles : flapping wing propulsion by Koay, Say Seng.

“…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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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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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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Design of pinned and rigid bolted connections using BS 5950:2000 and Eurocode 3 by Xie, Yunshen.

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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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“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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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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Performance and flight dynamics characteristics of a variable sweep wing aircraft by Chong, Zi Wei.

“…The parameters of the wings that are altered across these different morphing stages are wing root chord, tip chord and aspect ratio. …”
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Determination of operating point for a propulsive wing UAV using CFD by Chan, Chee Shuan

“…This report seeks to determine the operating point of a 2D propulsive wing UAV using CFD. CFD simulations were performed using a 2D RANS k-ε turbulence model and the rotating flow was captured using the moving reference frame method. …”
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Synaptic element for neuromorphic computing using a magnetic domain wall device with synthetic pinning sites by Jin, Tianli, Gan, Weiliang, Tan, Funan, Sernicola, Nicolo Roberto, Lew, Wen Siang, Piramanayagam, S. N.

“…The control of the domain wall motion with the synthetic pinning sites is demonstrated to be a reliable technique for neuromorphic applications.…”
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The natively disordered loop of Bcl-2 undergoes phosphorylation-dependent conformational change and interacts with Pin1 by Bharatham, Nagakumar, Chia, Joel, Mu, Yuguang, Baek, Kwanghee, Yoon, Ho Sup, Kang, CongBao

“…Finally, we show that the phosphorylated peptides of the Bcl-2 loop can bind Pin1, further substantiating the phosphorylation-mediated conformation change of Bcl-2.…”
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An autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin by Lim, Chee Wei.

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Simulation of suppression of vortex breakdown over delta wings by vortex filament method by Lewpiriyawong Nuttawut.

“…The purpose of perturbing the vortex core is to delay or suppress vortex breakdown over delta wings.…”
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