1996
DOI: 10.1016/1359-8368(95)00027-5
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Thickness optimization for maximum buckling loads in composite laminated plates

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Cited by 17 publications
(10 citation statements)
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“…This also agrees well with the thickness distribution found by Joshi and Biggers. 13 As an example, two design layers and their balanced counterpart are shown in Figure 7: the layer at the outside, which completely covers the plate, is shown on the left. Almost no steering is observed, and the angles are almost ±45…”
Section: Resultsmentioning
confidence: 99%
“…This also agrees well with the thickness distribution found by Joshi and Biggers. 13 As an example, two design layers and their balanced counterpart are shown in Figure 7: the layer at the outside, which completely covers the plate, is shown on the left. Almost no steering is observed, and the angles are almost ±45…”
Section: Resultsmentioning
confidence: 99%
“…The design objective was the maximization of the uniaxial buckling load by optimally, determining the fiber orientations. Joshi and Biggers [22] determined optimal thickness distributions over the plate that yields maximum uniaxial and biaxial buckling loads. Isotropic plates and composite laminated plates were modeled using variable thickness, shear deformable and finite plate elements.…”
Section: Introductionmentioning
confidence: 99%
“…Different design methods have been employed to optimize the structural performances of the laminated composites against buckling load in terms of design variables such as the fiber orientations and stacking sequence . In this context, genetic algorithms (GA) as a promising method have attracted attention to maximize the buckling strength of composite plates .…”
Section: Introductionmentioning
confidence: 99%
“…In addition, Setoodeh and Shojaee [23] proposed a methodology named TW-DQ for application of DQM to general quadrilateral plates and particularly examined the nonlinear free vibration analysis of CNTRC quadrilateral thin plates based on classical plate theory. Different design methods have been employed to optimize the structural performances of the laminated composites against buckling load in terms of design variables such as the fiber orientations and stacking sequence [24][25][26][27][28][29][30][31][32][33][34][35][36]. In this context, genetic algorithms (GA) [33] as a promising method have attracted attention to maximize the buckling strength of composite plates [24,32].…”
Section: Introductionmentioning
confidence: 99%