34th Congress of the International Council of the Aeronautical Sciences

03.4 - Applied Aerodynamics

AERODYNAMIC SHAPE OPTIMIZATION OF FILLETED INTERSECTIONS WITH SURFACE MESH DEFORMATION

H.M. Hajdik¹, A. Yildirim¹, J.R.R.A. Martins¹; ¹University of Michigan, United States

Component intersections are a persistent challenge in aerodynamic design. In this work, we present a method based on inverse distance warping to deform a fillet between two components for the minimum drag design. We show that this is tractable within gradient-based aerodynamic shape optimization and results in lower drag designs than those optimized without changing the intersection region.


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