Crash Simulation Of A Composite Unmanned Aerial Vehicle Fuselage by Yidris, Noorfaizal

“…The simulation of the composite fuselage sections was carried out, refined several times and validated with the experimental results. …”
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Crush simulation of woven c-glass/epoxy unmanned ariel vehicle fuselage section by Yidris, Noorfaizal, Zahari, Rizal, Abang Abdul Majid, Dayang Laila, Mustapha, Faizal, Hameed Sultan, Mohamed Thariq, Mohd Rafie, Azmin Shakrine

“…A quasi-static crush analysis of an unmanned aerial vehicle (UAV) fuselage section made of woven c-glass/epoxy has been conducted using the finite element simulation via ABAQUS. …”
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Prediction of fatigue life of aluminum 2024-T3 at low temperature by finite element analysis by Mazlan, Shahan, Yidris, Noorfaizal, Zahari, R., Gries, E., Abang Abdul Majid, Dayang Laila, Ahmad, Kamarul Arifin

“…The change in material properties at low temperature has always been one of the concerned design factors in aircraft industries. The wings and fuselage are repeatedly exposed to sub zero temperature during cruising at high altitude. …”
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Experimental and numerical analysis of fatigue life of aluminum Al 2024-T351 at elevated temperature by Mazlan, Shahan, Yidris, Noorfaizal, Seyed Saeid, Rahimian Koloor, Petrů, Michal

“…Structural parts such as fuselage, wings, aircraft turbines and heat exchangers are required to work safely at this working condition even with decreasing fatigue strength and other properties. …”
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