Summary The turbulence models implemented into the FLOWer code are briefly characterized, considering their basic equations and emphasizing their differences with respect to their aimed at field of application. The influence of the models on the flow solution is demonstrated for two simple test cases, the flow around the RAE 2822 airfoil, representing transonic conditions, and the flow around the Aérospatiale A airfoil, representing high-lift conditions. Results for industrially more relevant test cases of the flow around two different wing-body configurations and a three-element airfoil are presented, confirming the findings for the simple geometries at least under transonic conditions. From this, recommendations for the choice of suitable models are derived.
Turbulence Models in FLOWer
2005-01-01
15 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2005
|Turbulence models in pulsating flows
AIAA | 2001
|Turbulence Models in Pulsating Flows
AIAA | 2002
|Development of relaxation turbulence models
TIBKAT | 1976
|Collaborative testing of turbulence models
AIAA | 1991
|