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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Domain wall pinning through nanoscale interfacial Dzyaloshinskii-Moriya interaction by Kumar, Durgesh, Chan, Jianpeng, Piramanayagam, S. N.

“…We have also studied pinning in a device with five successive pinning sites. …”
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1,3,5-triazaspiro[5.5]undeca-2,4-dienes as selective Mycobacterium tuberculosis dihydrofolate reductase inhibitors with potent whole cell activity by Yang, Xuan, Wedajo, Wassihun, Yamada, Yoshiyuki, Dahlroth, Sue-Li, Neo, Jason Jun-Long, Dick, Thomas, Chui, Wai-Keung

“…This study aimed to develop selective M. tuberculosis DHFR inhibitors using rationale scaffolding design and synthesis, phenotype-oriented screening, enzymatic inhibitory study, whole cell on-target validation, molecular modeling, and in vitro DMPK determination to derive new anti-TB agents. 2,4-diamino-1-phenyl-1,3,5-triazaspiro[5.5]undeca-2,4-dienes 20b and 20c were identified as selective M. tuberculosis DHFR inhibitors, showing promising antimycobacterial activities (MIC50: 0.01 μM and MIC90: 0.025 μM on M. tuberculosis H37Rv). …”
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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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Search for long-lived particles decaying to final states with a pair of muons in proton-proton collisions at √𝑠 = 13.6 TeV by Hayrapetyan, A., Tumasyan, A., Adam, W., Andrejkovic, J. W., Bergauer, T., Chatterjee, S., Damanakis, K., Dragicevic, M., Hussain, P. S., Jeitler, M., Krammer, N., Li, A., Liko, D., Mikulec, I., Schieck, J., Schöfbeck, R., Schwarz, D.

“…An inclusive search for long-lived exotic particles (LLPs) decaying to final states with a pair of muons is presented. …”
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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

“…Of note is the persisting of attached flow regions over certain areas of the wing which is posited to be due to the imparting of momentum from long separation bubbles over saddle-chords. …”
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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 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 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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Long contraction scour by Koh, Chun Wei

“…Hence, the objective of this study is to study the phenomenon of long and gradual contraction scouring in an open channel flow. …”
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5G : The 5th Generation Mobile Networks / by Trick, Ulrich, author 655465, Walter de Gruyter GmbH (Online service) 655461

Subjects: “…5G mobile communication systems…”
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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

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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Vehicular localization using 5G V2X by Pan, Yongqi

“…This project will discuss on different vehicle positioning methods related to the 5G V2X. Besides, a simulation solution using mmWave signals to complete vehicle positioning will be given. …”
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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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