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This work investigates the effect of span-length on how the loads and flow structure are changed as a swept wing is undergoing dynamic stall.

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This page is a summary of: Effect of Aspect Ratio on Swept-Wing Dynamic Stall, AIAA Journal, October 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j063039.
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