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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End of the line by Chia, Wei Ting

“…My Final Year Project “End of the Line” is an experimental effort to create an expressive piece of game design, writing and drawing to explore the possibilities of creating a narrative driven card game that combines elements of walking simulators, interactive fiction, and strategic card games. …”
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Frail Line by Er, Kia Hui, Ong, Grace Xi Wei, Ho, Baofei, Tan, Jit Quan, Boithar, Faizal

“…Frail Line is a story about the changed dynamics of a father-daughter relationship after a separation of many years. …”
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Place recognition using line-junction-lines in urban environments by Tang, Xiaoyu, Fu, Wenhao, Jiang, Muyun, Peng, Guohao, Wu, Zhenyu, Yue, Yufeng, Wang, Danwei

“…Bag- of-Words (BoW) -based approach is the most popular solution due to its efficiency and robustness. We propose to use Line- Junction-Line (LJL) to build a BoW for place recognition in urban environments. …”
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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.

“…The wing used was a straight wing of airfoil NACA 0012. …”
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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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The design of a rail-to-rail output swing using a nested-current-mirror single-stage amplifier with a high PSRR by Goh, Zhi Xian

“…The project is to design a Nested – Current – Mirror Operational Amplifier with Rail – to – Rail Output swing. The design is with reference to the paper written by Yan, Mak, Laws, Martins and Malobeti (2015), which consist of the basic structure of the Nested – Current – Mirror Operational Amplifier with a single output. …”
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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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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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