Hybrid RANS/LES simulation of a space launcher using an high order finite volume scheme and grid intersections technique
Grégoire Pont  1, @  , David Puech  2  , Pierre Brenner  1  
1 : Airbus Defence & Space  (ADS)  -  Website
AIRBUS Defence & Space
61 Route de Verneuil 78130 Les Mureaux -  France
2 : Airbus Defence & Space
AIRBUS Defence & Space
Subject : : Oral
Topics : Session 8 - A : High speed flow
PDF version :  PDF version
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