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Last Updated: October 3, 2026
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Here we minimize the drag of a rectangular wing Dr. John Jasa is the main developer of an open-source aerostructural This shows the design variables that can be optimized in the MACH framework. The wing shape and planform variables also ... Presented by Eytan Adler Find the paper here: websites.umich.edu/~mdolaboratory/pdf/Adler2022a.pdf In the past, ... Two optimizations are shown: weight minimization (left) and fuel burn minimization (right). More details on this paper: ... A loop algorithm was developed. It updates cross-sections iteratively until the whole mdolab.engin.umich.edu/content/high-aspect-ratio-wing-design-optimal-aerostructural-tradeoffs-next-generation-materials ...
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