01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)

RESEARCH ON AERODYNAMIC-STRUCTURAL RAPID EVALUATION AND OPTIMIZATION METHODS FOR JOINED-WING CONFIGURATIONS

X. Tang¹, B.G. Mi¹; ¹Northwestern Polytechnical University, China

This study develops an efficient aerostructural evaluation and optimization framework for Joined-Wing ISR aircraft. It combines fast aerodynamic models with structural analysis and multidisciplinary design optimization to balance accuracy and speed. This approach accelerates the design of high-performance aircraft and is applicable to other complex engineering systems requiring coupled analysis.

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DOI: 10.71945/icas2026_0577