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

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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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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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.…”

Part I: Synthesis of sex pheromone of the pine sawfly, Macrodiprion Nemoralis. Part II: Synthetic studies towards the total synthesis of iriomoteolide-1a by Chin, Yen Jin

“…In the first part of this thesis, an elegant display of the CuI-Tol-BINAP-catalyzed asymmetric conjugate addition is established in the total synthesis of sex pheromone of the pine sawfly, Macrodiprion Nemoralis (SRRS-1). The key features of our strategy are: (I) one-pot DIBAL-H reduction–Wittig olefination, (II) olefin cross metathesis of fragment A and fragment B, and (III) a CuI-Tol-BINAP-catalyzed asymmetric conjugate addition using Grignard reagents in good yields and excellent stereoselectivities. …”
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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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Jokowi After the First Term – Indonesia’s KPK : Clipping Its Anti-Corruption Wings? by Ng, Jefferson Jin Chuan

“…The Indonesian Parliament (DPR) and the President have discussed and approved an amendment clipping the wings of Indonesia’s independent anti-corruption agency. …”
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Learning Control of Fixed-Wing Unmanned Aerial Vehicles Using Fuzzy Neural Networks by Kayacan, Erdal, Khanesar, Mojtaba Ahmadieh, Rubio-Hervas, Jaime, Reyhanoglu, Mahmut

“…A learning control strategy is preferred for the control and guidance of a fixed-wing unmanned aerial vehicle to deal with lack of modeling and flight uncertainties. …”
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Lightweight mechanical amplifiers for rolled dielectric elastomer actuators and their integration with bio-inspired wing flappers by Lau, Gih-Keong, Lim, Hoong-Ta, Teo, Jing-Ying, Chin, Yao-Wei

“…Dielectric elastomer actuators (DEAs) are attractive for use in bio-inspired flapping-wing robots because they have high work density (specific energy) and can produce a large actuation strain. …”
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Design, fabrication, evaluation of low-speed UAV wing flap actuated with shape memory alloy by Seow, Aik Khiam

“…The project is a feasibility study to control a wing flap using SMA. Attention has been paid to conceptual design of actuation mechanisms, controllability of the actuation, and the response rate of SMA actuation. …”
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