Deep MinMax Networks by Lohmiller, Winfried, Gassert, Philipp, Slotine, Jean-Jacques

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Peperiksaan bantu bina daya tahan pelajar by Norizan, Yusof

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Design of spinal implant for an Asian population by Chou, Siaw Meng.

“…This report documents the design of a new cervical spinal implant. Eight-eight lateral radiographs of Asian cervical spinal were used for a morphological study.…”
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Solar UAV : design and fabrication of structural test rig for loading and testing a 7.5m half wing by Chua, Zac Zheng Xun.

“…The objective of the project was to design and manufacture a Solar UAV with wingspan of 17.5m, take-off weight of 60kg and having an endurance of 24 hours. …”
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Kerjasama Pelbagai Pihak Bina Ketahanan Hadapi Bencana Banjir by Ismail, Mohd Azril

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Investigation of wing rock on delta wing part 2 : dynamic characteristics by Wong, Charles Junxin.

“…This final year project focuses on the study of wing rock for delta wings at high angles of attack in a water tunnel. …”
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Insect inspired two-wing flapping wing micro air vehicle by Ma, Jiacheng

“…This report presents an in-depth study of the flight of the hawk moth Manduca Sexta, with the goal of replicating its wing motion for the design of a Micro Air Vehicle. …”
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RENCANA KEPUSTAKAWANAN : KUMPULAN FOKUS KHAS KEJURUTERAAN DAN SENI BINA / by Nik Masriza Zakaria, editor 607828, Aishahtun Abdul Majid, editor 655435, Azman Abdul Rahim, editor 655436, Kamariah Gono, editor 182892, Rohaida Mohamad Idaris, editor 655437, Engku Norulizati Engku Aziz, editor 655438, Muhamad Faizal Abd Aziz, editor 655439

Validation of wearable inertial sensors for spinal motion assessment by Tan, Crljen Yong Ming

“…Spinal musculoskeletal disorders (SMDs) are a common cause of pain and disability, affecting millions of people worldwide. …”
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UMNO perlu bina semula reputasi elak 'menang sorak, kampung tergadai' by Samsi, Abdul Hadi

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Investigation of wing rock on delta wing part 1 : flow field and hydrodynamic force analysis by Gan, Calvin Cheng Rui

“…This final year project focuses on the study of wing rock of delta wings at high angles of attack in a water tunnel. …”
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Understanding solar PV through the MinUS-C module grounded in the ADDIE instructional model by Muhamad Kamarul Azman Sulaiman, Lilia Halim, Nurazidawati Mohamad Arsad, Ruhizan Mohamad Yasin

“…The module's design involved five phases of the ADDIE model: analysis, design, development, implementation, and evaluation. …”
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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. …”
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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. …”
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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. …”
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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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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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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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