How to Calculate Lift and Drag of NACA 2412 Airfoil Wing in ANSYS | ANSYS Fluent Tutorial  | Part 2

How to Calculate Lift and Drag of NACA 2412 Airfoil Wing in ANSYS | ANSYS Fluent Tutorial | Part 2

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How to Calculate Lift and Drag of NACA 2412 Airfoil Wing in ANSYS | ANSYS Fluent Tutorial | Part 2
Buy PC parts and build a PC using Amazon affiliate links below - DDR5 CPU - https://amzn.to/47Hgqn6 DDR5 RAM - https://amzn.to/3SObJ6R Gen 4 SSD - https://amzn.to/49KgYL2 Mouse and Keyboard - https://amzn.to/47Ewjuz Motherboard - https://amzn.to/47hcsBS GTX 1650 GPU - https://amzn.to/47HM4Rl Cabinet - https://amzn.to/47J7TAh PSU - https://amzn.to/3MPuMK5 Download the geometry from this link - https://drive.google.com/file/d/1t6uh5Je6rGISAWgpg4fIdOwJEIDhqkc3/view?usp=sharing In this tutorial, we will learn how to do geometry preparation for a wing cad model and calculate lift and drag on the wing. In this video part 2, the procedure of geometry preparation, meshing, setting up boundary conditions, and calculating lift and drag results has been demonstrated. Kindly drop a mail at [email protected] for queries or support. https://youtu.be/W1eTcXMSfuk