34th Congress of the International Council of the Aeronautical Sciences

01.1 - Aircraft Design and Integrated System (Basics and Theory)

FAST PARAMETRIC STRUCTURE MODELING FOR VARIETY OF AIRCRAFT CONFIGURATIONS

Y.-L. Yin¹, K.-S. Zhang¹, H.-L. Qiao¹, A.-L. Che¹, Z.-H. Han¹; ¹School of Aeronautics, Northwestern Polytechnical University, China

This work proposed a surface discretization method to attain fast parametric structure modeling for complete aircraft configurations. The geometric model is established in a discretized way at the beginning of parametric modeling process instead of being discretized after finite element (FE) analysis is started. Then FE meshing becomes faster and more likely to succeed, and the design zones can be easily grouped. It’s successfully applied in modeling supersonic transport, tailless fighter and flying-wing bomber.


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