Automated multi-fidelity aerodynamic design pipeline for a High-Lift STOL wing. Integrates Python (AeroSandbox) for parametric optimization, OpenVSP for 3D sizing, and Ansys Fluent (RANS) for high-fidelity physics validation.
A nonlinear 6-DOF flight dynamics simulator for STOL aircraft modeling distributed propulsion effects (Blown Wing), with real-time FlightGear SIL visualization.
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