Computational aerodynamics laboratory project implementing Hess-Smith panel method and Weissinger lifting-line theory for airfoil and wing analysis
-
Updated
Jan 22, 2026 - MATLAB
Computational aerodynamics laboratory project implementing Hess-Smith panel method and Weissinger lifting-line theory for airfoil and wing analysis
3D Vortex Lattice Method (VLM) implementation for a swept, tapered wing with elliptical loading comparison.
Add a description, image, and links to the wing-design topic page so that developers can more easily learn about it.
To associate your repository with the wing-design topic, visit your repo's landing page and select "manage topics."