GATUS
| Project | GATUS |
| Research Area | Engineering |
| Principal Investigator(s) | Vassilis Theofilis |
| Institution(s) |
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Abstract
The instability properties of the turbulent separated flow over aircraft airfoils at high angles of attack are studied through the solution of partial-derivative-based eigenvalue problems. The complex geometry and involved physics make it impossible to use simplified analysis, within the possibilities of personal computers. Massive parallelization is required then to obtain physical meaningful results, useful on the industrial field.
