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

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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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“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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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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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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Filmwise condensation of steam on sinusoidal pin fin arrays : effects of fin height and fin pitch by Ho, Jin Yao, Leong, Kai Choong, Wong, Teck Neng

“…An experimental investigation on the use of sinusoidal pin fins to enhance filmwise condensation of steam on vertical plates was carried out. …”
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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

“…Wind tunnel tests were then conducted on a 3D printed propulsive wing model to assess and confirm the general trends produced by CFD. …”
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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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Whose right, whose left? Analyzing the complexities of right-wing politics in Venezuela by Jiménez, M, Aveledo, GT

“…As authoritarianism and repression have increased and Venezuela’s socioeconomic decline has worsened, right-wing movements and factions have prioritized competitiveness through a centrist approach over an emphasis on ideological purity.…”

Mechanism of charge transfer and its impacts on Fermi-level pinning for gas molecules adsorbed on monolayer WS2 by Zhou, Changjie, Yang, Weihuang, Zhu, Huili

“…The phenomenon of Fermi-level pinning was discussed in light of the traditional and orbital mixing charge transfer theories. …”
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Experimental and numerical studies of pin-ended S960 ultra-high strength steel press-braked channel section columns by Ong, Shao Quan

“…The structural testing programme were performed on two nonslender plain channel sections and comprised detailed measurements of initial global and local geometric imperfections, as well as a total of 10 flexural buckling tests on pin-ended columns buckling about their minor axes. …”
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Comparison and validation of sensors for 3D and 2D motion capture to measure 10-pin bowling specific kinematics by Lim, Matthew Jing Long

“…Ten pin bowling is a competitive sport that requires athletes to score as many pins possible using a bowling ball. …”
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A combined numerical and experimental approach to investigations of body-freedom flutter on flying wings by Ang, Elijah Hao Wei

“…With the recent rise in the development of aircrafts with high aspect-ratio wings adopting lightweight flexible structures, these aircrafts become increasingly vulnerable to aeroelastic phenomena. …”
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