Main ANSYS CFX file to produce transient thrust and input power for a pitching airfoil with NACA 0012 cross-section
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下载链接：
https://dataverse.lib.virginia.edu/citation?persistentId=doi:10.18130/V3/XZ2YLD
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资源简介：
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.
提供机构：
University of Virginia Dataverse
创建时间：
2016-03-14
