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Main ANSYS CFX File to Produce Transient Thrust and Input Power for a Pitching Airfoil With NACA 0012 Cross-Section

Saadat, Mehdi; Haj-Hariri, Hossein
Format
Computer Resource; Online
Author
Saadat, Mehdi
Haj-Hariri, Hossein
Abstract
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.
Date Received
20140725
Published
2014-07-25
Copyright Not EvaluatedCopyright Not Evaluated
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