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In this section of the tutorial, the blade geometry is imported, a mesh is created around the blade and the Fluent solver is then used to find the aerodynamics loading on the blade and the fluid flow. Here is more information about the set-up. 

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 Finally, periodics are used to allow the visualization of results for three blades. . Here is an example of the results that can be obtained at the end of this tutorial.

Are you ready? Let's do this!

Go to Step 1: Pre-Analysis & Start-Up

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