Research Article
Evidence-Based Multidisciplinary Design Optimization with the Active Global Kriging Model
Table 7
Lower and upper limit of variables.
| Design variables | ā | Original (mm) | Boundary of variables |
| Thickness of rib 1 | | 1.0 | [1.0, 2.50] | Thickness of rib 2 | | 1.0 | [1.0, 2.50] | Thickness of rib 3 | | 1.0 | [1.0, 2.50] | Thickness of rib 4 | | 1.0 | [1.0, 2.50] | Blade wall thickness at root of blade cross section | | 1.70 | [1.69, 1.71] | | 1.69 | [1.69, 1.71] | | 1.69 | [1.69, 1.71] | Blade wall thickness at top of blade cross section | | 1.2 | [1.20, 1.25] | | 1.2 | [1.20, 1.25] | | 1.0 | [1.0, 1.05] |
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