Evaluation AC7-03: Difference between revisions

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==Influence of the Discretization Error with URANS==
==Influence of the Discretization Error with URANS==
The error intervals of total pressure heads were up to 4.8% for the finest grid. From an engineering point of view, these uncertainties are in an acceptable range for the design of a VAD. In addition, the uncertainty for the pressure head for the whole VAD (4.8%) is higher than for the rotor alone (1.7%). The reason for this could be that turbulent phenomena, e.g. detachment in the outlet guide vane, affect the pressure increase via the whole pump. Those effects may have a significant mesh sensitivity and thus affect the uncertainty of the pressure head for the entire VAD. Furthermore, the relatively small uncertainties for the pressure heads suggest that the grid resolution of UR-7 is fine enough to guarantee a grid-independent solution and no further grid refinement seems to be required for these results.


==Experimental Validation of URANS and LES==
==Experimental Validation of URANS and LES==

Revision as of 13:51, 8 November 2021

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Turbulent Blood Flow in a Ventricular Assist Device

Application Challenge AC7-03   © copyright ERCOFTAC 2021

Evaluation

Influence of the Discretization Error with URANS

The error intervals of total pressure heads were up to 4.8% for the finest grid. From an engineering point of view, these uncertainties are in an acceptable range for the design of a VAD. In addition, the uncertainty for the pressure head for the whole VAD (4.8%) is higher than for the rotor alone (1.7%). The reason for this could be that turbulent phenomena, e.g. detachment in the outlet guide vane, affect the pressure increase via the whole pump. Those effects may have a significant mesh sensitivity and thus affect the uncertainty of the pressure head for the entire VAD. Furthermore, the relatively small uncertainties for the pressure heads suggest that the grid resolution of UR-7 is fine enough to guarantee a grid-independent solution and no further grid refinement seems to be required for these results.

Experimental Validation of URANS and LES

Comparison of Different URANS methods




Contributed by: B. Torner — University of Rostock, Germany

Front Page

Description

Test Data

CFD Simulations

Evaluation

Best Practice Advice

© copyright ERCOFTAC 2021