Media Summary: 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 Participating solvers: XFOIL.
Xoptfoil Airfoil Optimization - Detailed Analysis & Overview
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 Participating solvers: XFOIL. Aiming for best L/D at Re=50k. Matlab script wrapped around Xfoil. Download the free version: Get a free 14 day trial: ... A short lecture I gave about aircraft design
