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Last Updated: October 1, 2026
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Here we minimize the drag of a rectangular wing Structural weight minimization of a tubular spar composed of 6-DOF finite elements. We apply tip loads and allow the Dr. John Jasa is the main developer of an open-source aerostructural L/D | CL = 1 : maximized CL_max : maximized dCL_max : minimized Participating solvers: XFOIL. This shows the design variables that can be Presented by Eytan Adler Find the paper here: websites.umich.edu/~mdolaboratory/pdf/Adler2022a.pdf In the past, ...
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