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posted on 2021-05-07, 11:28 authored by Ernnie BasriErnnie Basri, Adi Azriff Basri, Kamarul Arifin Ahmad, Mohamed Thariq Hameed Sultan, Faizal MustaphaFig. 1 Methodology of multi-layered composite lamination
Fig. 2 Fabrication process
Fig. 3 Lamination arrangement of composite in ANSYS module
Fig. 4 Simulation setup for tensile
Fig. 5 Simulation setup for flexural
Fig. 6 Wing configuration
Fig. 7 Grid dependency test
Fig. 8 Visualization of lamination
Fig. 9 Tensile stress vs strain of experiment and simulation
Fig. 10 Flexural extension vs time of experiment and simulation
Fig. 11 Result of total deformation of UAV wing under aerodynamic loading
Fig. 12 Result of stresses s1, s2 and s12 under aerodynamic load
Fig. 13 Principal stress sI under aerodynamic load
Fig 14 Tsai-Wu failure
