SimScale simulation projects by tnkadimeng | Page 1

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This project conducts a CFD analysis of a NACA 2412 airfoil subjected to airflow at a velocity of 75 m/s. The purpose of the simulation is to evaluate the aerodynamic performance of the airfoil, focusing on pressure distribution, velocity field, and the calculation of lift and drag forces. An incompressible flow model with the k-ω SST turbulence model is used to accurately capture the boundary layer effects and flow separation behavior. The setup includes a fluid domain extending 5 chord lengths upstream and downstream, with symmetry conditions applied on the top and bottom faces of the enclosure. Results will provide insights into the airfoil’s efficiency, highlighting areas for potential design optimization. - Copy

This project conducts a CFD analysis of a NACA 2412 airfoil subjected to airflow at a velocity of 75 m/s. The purpose of the simulation is to evaluate the aerodynamic performance of the airfoil, focusing on pressure distribution, velocity field, and the calculation of lift and drag forces. An incompressible flow model with the k-ω SST turbulence model is used to accurately capture the boundary layer effects and flow separation behavior. The setup includes a fluid domain extending 5 chord lengths upstream and downstream, with symmetry conditions applied on the top and bottom faces of the enclosure. Results will provide insights into the airfoil’s efficiency, highlighting areas for potential design optimization.

Tutorial project for a flow analysis of a pipe junction. The project only provides the geometry to start with. See our tutorials section to have a look at the step-by-step instructions to set up the simulation.

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.

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