Dynamic Stall Characteristics of a Pitching Swept Finite Aspect Ratio Wing
This research will investigate various swept wing models, designing the mechanism for their pitching motion and control, designing wind tunnel implementation, and performing data measurements and analysis using particle image velocimetry. A NACA0012 section with an aspect ratio of AR = 4, free strea...
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| Format: | Others |
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North Dakota State University
2021
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| Online Access: | https://hdl.handle.net/10365/31721 |