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.
Aerodynamic-structural analysis of a hybrid VTOL transition wing - NACA 0012/2415/4412 spanwise layout, XFLR5 panel method, 9-module Python performance model
Computational aerodynamics laboratory project implementing Hess-Smith panel method and Weissinger lifting-line theory for airfoil and wing analysis
Industrial aerodynamics case study predicting laminar-to-turbulent boundary-layer transition over a 3-D natural-laminar-flow aircraft wing (AETHER-NLF 25), using the UTSS multi-mechanism transition solver β includes geometry, mesh, solver outputs, figures, experimental validation, and the full report.
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
Collaborative aircraft-wing structural analysis covering loads, shear and bending, deflection, torsion, stress and buckling calculations in Python.
3D Vortex Lattice Method (VLM) implementation for a swept, tapered wing with elliptical loading comparison.
π¬οΈ Analyze aerodynamic properties using panel methods and lifting-line theory, facilitating effective airfoil and wing design for aerospace applications.
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