Research Article
Reconstruction of Wing Structure Deformation Based on Particle Swarm Optimization Ridge Regression
Table 2
Strain average of one strain point under 34 load cases.
| | Load case | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9 |
| | Strain average () | -4.01 | -5.89 | 0.24 | 73.19 | 202.15 | -4.69 | -2.08 | -4.51 | 68.18 | | Load case | 10 | 11 | 12 | 13 | 14 | 15 | 16 | 17 | 18 | | Strain average () | 204.47 | -2.45 | -1.57 | -5.71 | 69.85 | 203.07 | -1.01 | 1.95 | 0.30 | | Load case | 19 | 20 | 21 | 22 | 23 | 24 | 25 | 26 | 27 | | Strain average () | 105.25 | 310.38 | 278.88 | 269.24 | 272.83 | 178.18 | 166.10 | 164.03 | 9.72 | | Load case | 28 | 29 | 30 | 31 | 32 | 33 | 34 | | | | Strain average () | 3.25 | -3.36 | -5.77 | -186.71 | -155.38 | -314.31 | -212.65 | | |
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