wing-design

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.

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

Aerodynamic-structural analysis of a hybrid VTOL transition wing - NACA 0012/2415/4412 spanwise layout, XFLR5 panel method, 9-module Python performance model

Open-source UAV wing engineering platform combining parametric CAD, CAM, aerodynamics, FEA, optimisation, prototype validation, automation, and an interactive 3D GitHub Pages app.

Powered-lift STOL wing design using blown-flap theory, BEMT propeller modeling, and DEP aerodynamic optimization validated through CFD

Classical and computational aerodynamics from first principles in Python/NumPy: thin airfoil theory, a Hess–Smith panel method, Thwaites/Head boundary layer with Squire–Young drag, and a 3D vortex lattice method, each validated against exact solutions, classical theory and published NACA data.

Physics-informed generative inverse design of aeroelastic glider wings using airfoil and conditional VAEs

🌬️ 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.

Collaborative aircraft-wing structural analysis covering loads, shear and bending, deflection, torsion, stress and buckling calculations in Python.