Research Article
Improved Reliability-Based Optimization with Support Vector Machines and Its Application in Aircraft Wing Design
Table 2
Design variables of wing.
| | Design variables | (mm2) | (mm) | (mm) | (mm) | (kg) | |
| | Lower value | 50.0 | 1.0 | 1.0 | 1.0 | — | — | | Upper value | 700.0 | 2.0 | 1.0 | 2.0 | — | — | | Origin design | 300.0 | 1.5 | 1.5 | 1.5 | 88.529 | 1.125 | | Optimal design | 50, 56.5, 125.6, 221.0, 341.4, 483.8, 642.3 | 1.0 | 1.0 | 1.0 | 63.975 | 0.965 |
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