01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
HIGH-FIDELITY DATASET-BASED SHAPE AND STRUCTURE OPTIMIZATION FOR AIRCRAFT DESIGN
M. Maier¹, K. Sørensen-Libik², Ö. Petersson², C. Breitsamter¹; ¹Technical University of Munich (TUM), Germany ;²Airbus Defence and Space GmbH, Germany
High-fidelity aeroelastic dataset-based optimization leverages the sets of load conditions from the aerodynamic analysis to perform simultaneous structural analysis for the full flight envelope. This reduces structural design risks significantly and enables robust optimizations, including the effect of elasticity on performance as well as stability and control in the aircraft design process.
DOI: 10.71945/icas2026_0042