2016
DOI: 10.1016/j.compstruct.2016.02.034
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Stacking sequence optimization for maximum buckling load of composite plates using harmony search algorithm

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Cited by 36 publications
(10 citation statements)
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“…14 The critical buckling load is quite sensitive to the anisotropic properties of laminated composite plates, and many studies have treated lay-up and fiber orientation as design variables for buckling optimization of composite plates. 1518 From the above descriptions, fundamental frequency and buckling load are the critical factors in the design of laminated composite structures, and in the present work, they are also the main concerns to be maximized for optimal lay-up designs.…”
Section: Introductionmentioning
confidence: 88%
“…14 The critical buckling load is quite sensitive to the anisotropic properties of laminated composite plates, and many studies have treated lay-up and fiber orientation as design variables for buckling optimization of composite plates. 1518 From the above descriptions, fundamental frequency and buckling load are the critical factors in the design of laminated composite structures, and in the present work, they are also the main concerns to be maximized for optimal lay-up designs.…”
Section: Introductionmentioning
confidence: 88%
“…Because of the advantages of using laminated composites in structural applications, their performance has been researched extensively. In these fields, various optimization studies have been carried out to maximize the performance of these structures while reducing cost [6][7][8][9][10][11][12][13][14][15][16][17][18][19][20][21][22][23]. Vo-Duy et al [24,25] presented the weight minimization and natural frequency maximization problems of laminated plates using an adaptive elitist differential evolution algorithm treating the ply thicknesses, fiber orientations, and the fiber volume fractions as the variables of optimization.…”
Section: Introductionmentioning
confidence: 99%
“…Kaveh et al [31] investigated the application of the BBO algorithm in stacking sequence optimisation of laminated composite plates for various load cases and aspect ratios to maximise the buckling load factor. HS was utilised by Almeida et al [32] to optimise the buckling load factor of the balanced laminated composite plate under compressive in-plane loads. Akcair et al [33] applied DE and SA to optimise the buckling load factor of the laminated composite plate under different increments in fibre orientations.…”
Section: Introductionmentioning
confidence: 99%