Les for near field wakes behind junction of wing and plate
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.
Key wordsLES tip vortex turbulence compact scheme
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