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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High-spin impurities and surface acoustic waves in piezoelectric crystals for spin-lattice coupling by Magnusson, E

“…<p>In this thesis we investigate various aspects of SAW devices and strain sensitive spin species in ZnO and LiNbO₃ for coupling surface acoustic waves to spin ensembles.…”

Hole spin helix : anomalous spin diffusion in anisotropic strained hole quantum wells by Sacksteder, Vincent E., Bernevig, B. Andrei

“…We obtain the spin-orbit interaction and spin-charge coupled transport equations of a two-dimensional heavy hole gas under the influence of strain and anisotropy. …”
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A meditation : spinning tops by Teong, Derek Shi Hong

“…A Meditation: Spinning Tops is a project that focuses on infusing a few key concepts embodied by the spiral into spinning tops, both in the actual object itself, as well as in the act of spinning the tops. …”
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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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Filmwise condensation of steam on pin fin arrays fabricated by selective laser melting by Ho, Jin Yao, Leong, Kai Choong

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Spin multistability in dissipative polariton channels by Bozat, Ö., Savenko, I. G., Shelykh, Ivan A.

“…We investigate the effect of the temperature and the longitudinal-transverse splitting on the spin (polarization) multistability and hysteresis arising from the polarization-dependent polariton-polariton interaction. …”
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Spin carbon nanotubes into CNT fibers by Lim, Johnathan See Kwan.

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Ballistic spin transport in exciton gases by Kavokin, A. V., Vladimirova, M., Jouault, B., Liew, Timothy Chi Hin, Leonard, J. R., Butov, L. V.

Subjects: “…Spin transport…”
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Spin structures and AdS4 holography by Bobev, N, Bomans, P

“…For a generic choice of the orbifold action, there is only one spin structure that preserves invariant Killing spinors. …”

Spin structures and AdS4 holography by Bobev, N, Bomans, P

“…For a generic choice of the orbifold action, there is only one spin structure that preserves invariant Killing spinors. …”

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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MENGAPA YAHUDI INGIN KUASAI BAITULMUQADDIS? : Benarkah matlamat yahudi menawan Baitulmuqaddis untuk bina istana dajjal? / by Abu Muhammad Arafah Adha, 1951-, author 644018