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2Â Geometries
2Â Meshes
5Â Simulation setups
7Â ResultsCFD analysis of NACA 2412 tapered wing to determine lift, drag and pressure distribution at various angles of attack. Part of aerospace engineering portfolio.
srikruti created this project
about 2 months ago
2Â Geometries 2Â Meshes 5Â Simulation setups 7Â ResultsCFD analysis of NACA 2412 tapered wing to determine lift, drag and pressure distribution at various angles of attack. Part of aerospace engineering portfolio.
by slilbaekslilbaek
