Computational aerodynamics laboratory project implementing Hess-Smith panel method and Weissinger lifting-line theory for airfoil and wing analysis

AeroShape aims to become a fully comprehensive 3D geometry engine for all aircraft components (fuselages, nacelles, etc.), capable of generating geometry representations for various aerodynamic structural analyses, CAD export, and design optimization.

🌬️ Analyze aerodynamic properties using panel methods and lifting-line theory, facilitating effective airfoil and wing design for aerospace applications.

3D Vortex Lattice Method (VLM) implementation for a swept, tapered wing with elliptical loading comparison.