Numerical study of airfoil stall cells using a very wide computational domain

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...

Detaylı Bibliyografya
Asıl Yazarlar:	Manni, L, Nishino, T, Delafin, P
Materyal Türü:	Journal article
Baskı/Yayın Bilgisi:	Elsevier 2016

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