Wing Optimisation for a Hypothetical Electric General Aviation Aircraft
Python-driven optimisation workflow selecting from 170+ NACA airfoils and refining a 3D wing in XFLR5, reaching a cruise glide ratio of 31.46.
Python-driven optimisation workflow selecting from 170+ NACA airfoils and refining a 3D wing in XFLR5, reaching a cruise glide ratio of 31.46.