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Application of mesh-free methods in the wing rigidity analysis to support automation of UAV design

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This framework integrates mesh-free methods and generative engineering to enhance aerodynamic efficiency and structural analysis for UAVs.

The developed computational framework significantly reduces design evaluation time, achieving individual assessments in about 20 seconds.
Integration of mesh-free methods enhances structural analysis while maintaining precision, improving design efficiency by 2-3 orders of magnitude.
Using meta-models from prior CFD studies allows effective estimation of aerodynamic loads, enabling rapid evaluation and optimization.
Future work aims to validate finite element models and incorporate aeroelastic coupling into the framework for complex UAV configurations.

Pasko et al. (2025) studied this question.

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This framework integrates mesh-free methods and generative engineering to enhance aerodynamic efficiency and structural analysis for UAVs.