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Last Updated: October 22, 2026
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Aiming for best L/D at Re=50k. Matlab script wrapped around Xfoil. In this example, we start with a circle, and use aerodynamic shape Minimize drag coefficient at single cruise flight condition subject to a thickness and trailing edge angle constraint. Matlab's fmincon ... L/D | CL = 1 : maximized CL_max : maximized abs(dCL_max - 0.05) : minimized Participating solvers: XFOIL. We have developed a ParaView-based graphical user interface (GUI) to facilitate the
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