04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity

AN AUTOMATED PARAMETRIC FRAMEWORK FOR EARLY-STAGE STRUCTURAL DESIGN AND OPTIMIZATION OF COMPOSITE AIRFRAMES

N. Ziakos, Spain; A. Cini, Spain

This paper presents an automated parametric framework for early-stage structural design and optimization of composite airframes. The approach integrates parametric finite-element model generation with physics-based structural analysis and data-efficient surrogate-assisted optimization, enabling systematic exploration of wing and fuselage structural designs.

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DOI: 10.71945/icas2026_0948