Abstract
Large eddy simulation with high-order accuracy and high resolution has been performed on the tip vortex shed from a rectangular half-wing with a NACA 0012 airfoil section and a rounded wing tip. The formation of the tip vortex and its initial development in the near field are studied and analyzed in details.
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References
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Project supported by the Office of Naval Research, USA (Grant No: N00014-03-1-0492).
Biography :Jiang, Senior Research Associate; Cai, PhD Student; Liu, Professor
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Jiang, L., Cai, J. & Liu, C. Les for near field wakes behind junction of wing and plate. J Hydrodyn 18 (Suppl 1), 265–268 (2006). https://doi.org/10.1007/BF03400457
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DOI: https://doi.org/10.1007/BF03400457