This project is prepared as part of CA course and it contains a study on the 2 dimensional Hess-Smith panel method (HSPM) for a cambered airfoil, NACA 1408.
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Updated
Jan 12, 2023 - MATLAB
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computational-aerodynamics
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Nastran helper code to design and analyse the aeroelastic response of a wing, plot the pannels for the doubblet lattice method and the FEM mesh.
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Updated
May 23, 2024 - MATLAB
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