SEGOMOE-Derived Pareto Wing (SDPW-01) 模型预览

GrabCAD 模型信息

SEGOMOE-Derived Pareto Wing (SDPW-01) · 模型 165334

作者:Dharun Narayan Venkatesh

This geometry is the result of a multi-objective aerodynamic optimization process driven by the SEGOMOE algorithm. Rather than being manually designed, the configuration emerges from iterative exploration of the design space, converging toward a Pareto-optimal balance between competing objectives such as drag reduction, lift distribution, and geometric smoothness. The final form is a blended flying wing with a continuous surface transition and an integrated central body, shaped entirely through algorithmic evolution. Local thickness variations and curvature distributions reflect constraint handling and trade-off resolution performed during optimization. The triangulated mesh represents a simulation-ready state, suitable for CFD validation and further refinement. This model is intended as a proof-of-concept for algorithm-driven aerodynamic design workflows.

格式
Rendering、STL
分类
Aerospace、Just for fun、Military
标签
未标注
数据更新
2026-09-18T04:59:53Z
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