Design of single-span medium-to-high strength concrete deep beams by Tan, Kang Hai., Kong, Fung Kew.

“…This project is to design of single-span medium-to-high strength concrete deep beams.…”
Get full text

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. …”
Get full text

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. …”
Get full text

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. …”
Get full text

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. …”
Get full text

Creep and thermal response of long span prestressed concrete integral abutment bridge / by Akilu Muhammad, 1972-, author 609880, Redzuan Abdullah, supervisor 558354, Mohamad Salleh Yassin, supervisor 304475, Fakulti Kejuruteraan Awam 8022

Creep and thermal response of long span prestressed concrete integral abutment bridge / by Akilu Muhammad, 1972-, author 609880

Objects of Collaboration: Roles and Sequences of Objects in Spanning Knowledge Group Boundaries in Design by Brubaker, Eric R, Sheppard, Sheri D, Hinds, Pamela J, Yang, Maria C

“…<jats:title>Abstract</jats:title> <jats:p>Spanning knowledge group boundaries is both a source of and barrier to design performance and innovation. …”
Get full text

Objects of Collaboration: Roles of Objects in Spanning Knowledge Boundaries in a Design Company by Brubaker, Eric R, Sheppard, Sheri D, Hinds, Pamela J, Yang, Maria C

“…These findings are significant because they clarify the roles of objects in cross-boundary design work and suggest ways for designers to more effectively use objects to span knowledge boundaries.</jats:p>…”
Get full text

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. …”
Get full text

Micro air vehicles : flapping wing propulsion by Koay, Say Seng.

“…The wing used was a straight wing of airfoil NACA 0012. …”
Get full text

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. …”
Get full text

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. …”
Get full text

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. …”
Get full text

Investigation and fabrication of tiltrotors/tiltwings with morphing wing mechanisms by Hon, Shah Kiat.

Get full text

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. …”
Get full text

Flow distribution and mass removal in floating treatment wetlands arranged in series and spanning the channel width by Yamasaki, Taís N, Walker, Christopher, Janzen, Johannes G, Nepf, Heidi

Get full text

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.

Subjects: Get full text

“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. …”
Get full text
Get full text

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. …”
Get full text