Abstract
In this work, a surrogate assisted optimization method is utilized to optimize buckling loads of variable stiffness composites made by fiber steering. To improve the efficiency of optimization procedure, an expected improvement criterion is employed. Moreover, considering uncertainties of the fiber placement, a robust surrogate, least square support vector regression (LSSVR) considering empirical and structural risks is integrated with the expected improvement (EI) criterion and applied to two applications. The first case is the fiber path design of a variable stiffness plate under the compression load. The second one is the fiber path design of a variable stiffness cylinder under the bending load. According to results of the optimization, the buckling load of the variable stiffness plate has 52.63% improvement than the constant stiffness plate and 24.3% improvement than the quasi-isotropic plate. The buckling load of the variable stiffness cylinder has 40.22% improvement than the constant stiffness cylinder and 31.25% improvement than the quasi-isotropic cylinder. Furthermore, to verify the robustness of optimal design variables for the variable stiffness cylinder, the perturbed optimum design is presented and demonstrates that the results are reliable.
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Notes
N denotes the number of the sample points
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Acknowledgements
This work has been supported by Project of the Program of National Natural Science Foundation of China under the Grant Numbers 11172097, 11302266 and 61232014.
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Appendix
Appendix
There are three criteria of the surrogate as shown in the literature (Jin et al. 2001).
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a)
R square
$$ {R}^2=1-\frac{{\displaystyle \sum_{i=1}^n{\left({y}_i-{\tilde{y}}_i\right)}^2}}{{\displaystyle \sum_{i=1}^n{\left({y}_i-\overline{y}\right)}^2}} $$(15) -
b)
relative average absoluteerror (RAAE)
$$ RAAE=\frac{{\displaystyle \sum_{i=1}^n\left|{y}_i-{\tilde{y}}_i\right|}}{n* STD} $$(16) -
c)
relative maximum absolute error (RMAE)
$$ RAAE=\frac{ \max \left(\left|{y}_1-{\tilde{y}}_1\right|,\left|{y}_2-{\tilde{y}}_2\right|,\dots, \left|{y}_n-{\tilde{y}}_n\right|\right)}{STD} $$(17)In this study, R 2 is not considered as the criterion of the surrogate due to small size of samples in practical engineering problems. RAAE indicates the overall accuracy of a surrogate over the entire design space. A high RMAE value indicates a large error in a region of the design space.
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Ye, F., Wang, H. & Li, G. Variable stiffness composite material design by using support vector regression assisted efficient global optimization method. Struct Multidisc Optim 56, 203–219 (2017). https://doi.org/10.1007/s00158-017-1658-8
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DOI: https://doi.org/10.1007/s00158-017-1658-8