Determining lift and drag coefficient of NACA 4415 airfoil at different angles of attack

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Determining lift and drag coefficient of NACA 4415 airfoil at different angles of attack

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🛩️ NACA 4415 Airfoil: Lift and Drag Coefficient Analysis
Explore the aerodynamic intricacies of the NACA 4415 airfoil in this video! We determine the lift and drag coefficients at various angles of attack, providing valuable insights for aviation enthusiasts and engineering enthusiasts alike. 📊✈️
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Пікірлер: 6

@minahilnadeem9817 4 ай бұрын

does the vectors' sign for coefficient of lift and drag change for negative angle of attack?

@user-id1ty3vr7w 2 жыл бұрын

How to apply the angle of attack to calculate the momentum coefficient?

@Adroius 7 ай бұрын

I think changing the vector of the lift and drag report is a mistake isnt it?

@Holzmichie Жыл бұрын

Is there a way to automate this without having to rotate the airfoil and remeshing everytime ?

@Alexpontecrv Жыл бұрын

You can define the inlet velocity in vectors, by adding X and Y depending on the angle of attack, you can simulate the airfoil in other AOA without having to change the geometry or mesh.

@khuder Жыл бұрын

Parameterization and Design Exploration: ANSYS provides tools for parameterizing the airfoil geometry, allowing you to define key parameters such as thickness, camber, and chord length. By setting up a parameterized model, you can create a design exploration study within ANSYS Workbench or ANSYS DesignXplorer. This enables you to automatically vary the parameter values and evaluate the performance of different airfoil configurations without the need for manual rotation and remeshing.