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Mohd Firdaus Bin Abas
Mohd Firdaus Bin Abas
Universiti Putra Malaysia
Wing
Leading edge
Stiffness
Aerodynamics
Finite element method
3
Papers
46
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Conceptual design and simulation validation based finite element optimisation for tubercle leading edge composite wing of an unmanned aerial vehicle
2019
Journal of materials research and technology
Ernnie Illyani Basri
Faizal Mustapha
Mohamed Thariq Hameed Sultan
Adi Azriff Basri
Mohd Firdaus Bin Abas
Mohd Shukry Abdul Majid
Kamarul Arifin Ahmad
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Citations (4)
Performance analysis of composite ply orientation in aeronautical application of unmanned aerial vehicle (UAV) NACA4415 wing
2019
Journal of materials research and technology
Ernnie Illyani Basri
Mohamed Thariq Hameed Sultan
M. Faizal
Adi Azriff Basri
Mohd Firdaus Bin Abas
M.S. Abdul Majid
J. S. Mandeep
Kamarul Arifin Ahmad
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Citations (7)
Flapping wing micro-aerial-vehicle: Kinematics, membranes, and flapping mechanisms of ornithopter and insect flight
2016
Chinese Journal of Aeronautics
Mohd Firdaus Bin Abas
Azmin Shakrine Mohd Rafie
H. Yusoff
Kamarul Arifin Ahmad
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Citations (35)
1