Numerical study of airfoil stall cells using a very wide computational domain
The formation of stall cells over a NACA 0012 airfoil at a Reynolds number of one million has been investigated numerically, using unsteady Reynolds-averaged Navier–Stokes (URANS) and delayed detached-eddy simulation (DDES) approaches. The simulations are performed with a very wide computational dom...
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| 格式: | Journal article |
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Elsevier
2016
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