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Main ANSYS CFX file to produce transient thrust and input power for a pitching airfoil with NACA 0012 cross-section
The main ANSYS CFX file is attached. The code was used to produce cycle-averaged thrust and input power coefficients for a pitching foil with NACA 0012.
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Record · ID 1042369
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Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive