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2017
DOI: 10.1007/s00158-017-1683-7
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Optimal design of computer experiments for surrogate models with dimensionless variables

Abstract: This paper presents a method for constructing optimal design of experiments (DoE) intended for building surrogate models using dimensionless (or non-dimensional) variables. In order to increase the fidelity of the model obtained by regression, the DoE needs to optimally cover the dimensionless space. However, in order to generate the data for the regression, one still needs a DoE for the physical variables, in order to carry out the simulations. Thus, there exist two spaces, each one needing a DoE. Since the d… Show more

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Cited by 9 publications
(5 citation statements)
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References 41 publications
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“…fr,1 for the initial state without fracture, fr,2 after cracking on the entire thickness, fr,3 after delamination of 25% of the surface. The VPLM method [41] and its associated computer DoE plans [42] are used to obtain the approximate analytical expressions of ! for states 2 and 3.…”
Section: B Analytical Computations Of the Elastic Energy And Mean Enmentioning
confidence: 99%
“…fr,1 for the initial state without fracture, fr,2 after cracking on the entire thickness, fr,3 after delamination of 25% of the surface. The VPLM method [41] and its associated computer DoE plans [42] are used to obtain the approximate analytical expressions of ! for states 2 and 3.…”
Section: B Analytical Computations Of the Elastic Energy And Mean Enmentioning
confidence: 99%
“…While non-dimensionalization is by itself a variable transformation technique, it can further benefit by a combination with other techniques. Non-dimensionalization combined with exponential scaling transformations has been, for example, shown to be extremely effective at both reducing the dimensionality and improving the accuracy of surrogate models of mechatronic components over a large domain of variation of the input variables (multiple orders of magnitude) [26,92,142,175].…”
Section: Variable Transformation Techniquesmentioning
confidence: 99%
“…π pi = L a pi,0 j p a pi, j i (5) In the case where the dimensionless numbers π y and π di can be assumed constant, such as respectively the one representing the magnetic saturation and the one representing the diameter-length ratio for the motor, then the function f can be approximated by using scaling laws or similarity models [23,24]. Otherwise, when data is available, regression models [25,26] are used such as for modeling the propeller performance or landing gear structural analysis. A detailed description of the hypotheses and methods associated with these sizing models of drone components can be found in [14].…”
Section: Components Sizing Modelsmentioning
confidence: 99%
“…After several iterations, the final mass, M total, f inal calculated as sum of the different components must converge to this initial guess M total . This is expressed by the following inequality: M total ≥ M total, f inal (26) This condition is added to the global constraints, so that both results tend to a unique solution.…”
Section: Resolution Of Algebraic Loopsmentioning
confidence: 99%