Advanced Aerostructural Optimization Techniques for Aircraft Design

Table 3

Structural performance of the UAV predicted by different methodologies.

Prediction method	Maximum displacement, m	Mass of the wing, Kg	Maximum stress, MPa
CJSC	0.286	81.5623	93.24
Aly’s methodology	0.291	81.6183	86.56
GPU-accelerated RISM	0.291	81.6074	95.64
SAA	0.2871	81.6074	95.10