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. 2021 Sep 26;6(4):55. doi: 10.3390/biomimetics6040055

Table 4.

Values obtained from the sizing optimization and Finite Element Analysis for wing skins (a fixed and a moving wing).

Iterations Deformation Stress Original Skin
Thickness
Optimized Skin
Thickness
Weight Reduction
Ratio
Fixed Wing 4 98.85 mm 200 MPa 2 mm 0.995 mm 52.4%
Moving Wing 3 85.47 mm 199.7MPa 2 mm 0.84mm 58.3%