2019
DOI: 10.3390/ma12091412
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Vibration and Buckling Characteristics of Functionally Graded Graphene Nanoplatelets Reinforced Composite Beams with Open Edge Cracks

Abstract: This paper investigates the free vibration and compressive buckling characteristics of functionally graded graphene nanoplatelets reinforced composite (FG-GPLRC) beams containing open edge cracks by using the finite element method. The beam is a multilayer structure where the weight fraction of graphene nanoplatelets (GPLs) remains constant in each layer but varies along the thickness direction. The effective Young’s modulus of each GPLRC layer is determined by the modified Halpin-Tsai micromechanics model whi… Show more

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Cited by 45 publications
(9 citation statements)
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“…The multi-layer beam FE has been presented for buckling of laminated composite beam with improved element accuracy by considering the higher-order polynomials. 136 Further, Tam et al 137,138 have investigated the buckling behaviour of Gr-NCs with open edge cracks using first-order shear deformation theory (FSDT) and finite element method (FEM)-based analytical approaches. They concluded that the critical buckling load of the FG graphene platelet NCs structure was affected by the crack in the structure.…”
Section: Bucklingmentioning
confidence: 99%
“…The multi-layer beam FE has been presented for buckling of laminated composite beam with improved element accuracy by considering the higher-order polynomials. 136 Further, Tam et al 137,138 have investigated the buckling behaviour of Gr-NCs with open edge cracks using first-order shear deformation theory (FSDT) and finite element method (FEM)-based analytical approaches. They concluded that the critical buckling load of the FG graphene platelet NCs structure was affected by the crack in the structure.…”
Section: Bucklingmentioning
confidence: 99%
“…In general, aeronautical companies use FEM in structural analyses, vibrations, dynamic buckling and fluid flows in the fuselage, wing, turbine and other parts ( Figure 39) [284][285][286]. These analyses help determine the best geometry and material for each part of the aircraft, and understand how it will behave in service; for example, how the pressure and drag force will affect the aircraft during a flight [285,287].…”
Section: Aronauticalmentioning
confidence: 99%
“…By introducing GPLs to FGM materials, novel FG GPLs-reinforced composite (FG-GPLRC) structures have been developed recently and have since attracted extensive attention in both research and engineering communities [24]. Yang and his co-workers conducted pioneering studies on the mechanical behaviors of FG-GPLRC structures, such as beams [25][26][27][28], shells [29,30], and plates [31,32]. Focusing on the stability analysis of FG-GPLRC arches, the authors devoted extensive efforts to the investigation of such structures, including the characteristics of nonlinear static buckling, dynamic buckling, and free vibration for FG-GPLRC arches with different boundary conditions and external loads [33][34][35][36][37][38][39].…”
Section: Introductionmentioning
confidence: 99%