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The goal of this MICP (Mastering Industrial Codes and Parallelism) was to compare the behaviours of an aft swept wing with the one of a forward swept wing thanks to the industrial code Fluent. So two simple wings based on a NACA0012 profile were created and studied. This study included the discovery of the usage of Gambit to generate a profile and propagate a mesh (related in the associated manual), and the usage of Fluent to compute drag and lift coefficients.
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