Research Article

Advanced Aerostructural Optimization Techniques for Aircraft Design

Table 8

Optimization results validation.

CJSCGPU-accelerated RISMSAA

0.550 0.5500.4982
0.028490.028490.02846
−0.0642−0.0642−0.0641
Maximum stress (MPa)76.2577.7677.43
Maximum displacement (m)0.21780.21980.2162