Solar UAV : design and fabrication of structural test rig for loading and testing a 7.5m half wing by Chua, Zac Zheng Xun.

“…The objective of the project was to design and manufacture a Solar UAV with wingspan of 17.5m, take-off weight of 60kg and having an endurance of 24 hours. …”
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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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Investigation of wing rock on delta wing part 2 : dynamic characteristics by Wong, Charles Junxin.

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

“…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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Reactivating and reorganizing activity-silent working memory: two distinct mechanisms underlying pinging the brain by Yang, C, He, X, Cai, Y

“…Recent studies have proposed that visual information in working memory (WM) can be maintained in an activity-silent state and reactivated by task-irrelevant high-contrast visual impulses (“ping”). Although pinging the brain has become a popular tool for exploring activity-silent WM, its underlying mechanisms remain unclear. …”

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

“…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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Computational fluid dynamics of flapping wings by Ng, Eric Tee-Sang.

“…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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Adaptive wing and fuselage structure for UAVs by Truong, Ngoc Quoc Thang.

“…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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Analysis of flapping-wing compliant mechanism by Fam, Shi Jiez

“…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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Bi-stable mechanism for morphing wings by Yang, Jingjing

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

“…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.…”

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

“…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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A study of five derivatives markets in the Asia-Pacific Basin by Lai Ping, Lim, Yuan Yih, Sim, Maggie Yun Bee

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A comparative study on performance of five major bank in Singapore by Chow, Choy Leng, Pao, Ming Ern, Yeo, Keng Lee

“…Background information relating to the history, recent developments and operations were gathered to have a better understanding of the five selected banks, key indicators used to evaluate banks' performance are applied in our research. …”
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Investigation and fabrication of tiltrotors/tiltwings with morphing wing mechanisms by Hon, Shah Kiat.

“…This report included a historical study of tiltrotor/tiltwing developments and reviewed current developments in morphing aircrafts and V/STOL aircrafts. In order to provide a platform for researches and test-bedding of different technologies, a prototype was designed with low cost and ease of manufacturing in mind. …”
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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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