Open Access
表1
优化后结果与传统设计对比
| 结构 | 机翼最大应力/MPa | 机翼最大变形/mm | 机翼最大应变 | 质量/kg | 减重比率/% |
| 传统设计 | 318.2 | 241.5 | 0.006 76 | 5.41 | 31.6 |
| 优化后 | 256.7 | 203.6 | 0.005 51 | 5.56 | 29.7 |
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