Lat. Am. j. solids struct. vol.8 número4
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![Figure 2 Composite laminated plate with its boundary and load conditions. ⎧⎪⎪⎪⎪ ⎪⎨ ⎪⎪⎪⎪⎪ ⎩ OBJ = 10 − √ [ φ ( W t ∗ ) 2 ] 2 + [( 1 − φ ) ( C ∗ ) 2 ] 2 + 10 − 6 λ ∗ , if λ ∗ ≥ 1OBJ=(λ∗)2{10−√[φ(W t∗)2]2+[(1−φ) (C∗)2]2}, if λ∗<1 (1) C ∗ = C − C min](https://thumb-eu.123doks.com/thumbv2/123dok_br/18884413.423479/6.892.249.693.133.377/figure-composite-laminated-plate-boundary-load-conditions-obj.webp)
![Table 13 Results using GA-ANN – Example 2. Results Laminate [ 90 4 , ± 45, ( 90 2 , 0 2 ) 2 ] S ( N C max ) 0.989 ( N C crit ) 0.637 ( U max ) 26.6 × 10 − 3 m Fitness 23.42 GA Generations 47 Time 0.01 min.](https://thumb-eu.123doks.com/thumbv2/123dok_br/18884413.423479/11.892.266.571.145.320/table-results-using-example-results-laminate-fitness-generations.webp)
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