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Last Updated: October 1, 2026
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... development of the high-fidelity Here we minimize the drag of a rectangular wing with an aspect ratio of 10 while varying the aerodynamic twist and angle of attack ... This shows the design variables that can be Structural weight minimization of a tubular spar composed of 6-DOF finite elements. We apply tip loads and allow the As new airframe technologies and improved computational design tools allow for the aspect-ratio of aircraft wings to grow, the ... Presentation given at 2020 AIAA Aviation virtual forum. This presentation gives an overview of a low-fidelity method for rapid ... Presented by Eytan Adler Find the paper here: websites.umich.edu/~mdolaboratory/pdf/Adler2022a.pdf In the past, ... We take a look at how aerospace engineers are
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