Video builds on work by Cillian Thomas:
• NACA2412 Tutorial in A...
Video builds on work by Anthony T:
• ANSYS Fluent NACA 4412...
We show how to create a simple table of design points with a set of appropriate x- and y- velocities for inputs across angles of attack going from -8 degrees to +18 degrees for an inlet velocity of 33 m/s and Reynolds number of 2.2 million. We also use simple calculations of appropriate resultant forces to make sure we are determining a drag force parallel to the flow and a lift force normal to the flow. The simulated coefficients of lift and drag are in reasonable alignment with experimental data.
Негізгі бет Simulating NACA 2412 Airfoil over Varied Angles of Attack in Ansys Fluent with Verification
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