01 - Aircraft Design and Integrated Systems
A HIERARCHICAL STRUCTURAL MODEL FOR CONCEPTUAL DESIGN OF TRANSPORT AIRCRAFT WING
Y.K. Yinı, W.B. Songı; ıShanghai Jiao Tong University, China
The focus of the work is the development of a multi-level wing structural model, integrated with a parametric geometry model for aerodynamic analysis. The model includes shape definitions and multi-level internal structural definitions, which can adapt automatically to changes in aerodynamic shapes. The proposed method can meet different requirements for model fidelity, accuracy and efficiency.