The tutorial shows the ANSYS CFX procedure for NACA 4412 airfoil analysis.
Different angles of attack were investigated for a NACA 4412 airfoil by Varying the angle and a constant velocity to obtain both lift and drag forces. This project is being done using Design of Experiments (DOE) and Response surface (RS) techniques for Parameters set.
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To download project file, please click on the following link:
drive.google.com/file/d/1U7Eu...
Негізгі бет Learn How to Calculate Drag and Lift Forces on Airfoil in ANSYS CFX by using DOE
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