Simulates the Angle Of Attack (AOA) system of the Phantom F-4E fighter jet.
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Updated
Nov 7, 2022 - C++
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Simulates the Angle Of Attack (AOA) system of the Phantom F-4E fighter jet.
Investigates NACA 2412 airfoil aerodynamics using ANSYS Fluent CFD and MATLAB. Analyzes lift/drag coefficients across AoA to identify stall angle. Uses ~120k quad mesh, k-omega SST model. MATLAB applies Thin Airfoil Theory. CFD captures post-stall behavior (~12°). Includes animations, residuals, Cl/Cd plots.
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