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This project analyzes the aerodynamic performance of an airfoil under high-speed airflow conditions using Computational Fluid Dynamics (CFD). The airfoil is subjected to a velocity of 75 m/s to simulate realistic conditions for aerospace and wind energy applications. The analysis focuses on evaluating pressure distribution, velocity fields, and lift and drag forces to optimize airfoil efficiency and stability. The simulation uses the incompressible flow model with the k-ω SST turbulence model to capture boundary layer behavior accurately.
by slilbaekslilbaek
tnkadimeng created this project
about 1 year ago