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RANS Computations of tip Vortex Cavitation

The present study is related to the development of the tip vortex cavitation in Kaplan turbines. The investigation is carried out on a simplified test case consisting of a NACA0009 blade with a gap between the blade tip and the side wall. Computations with and without cavitation are performed using a RANS modelling and a transport equation for the liquid volume fraction. Compared with experimental data, the R ANS computations turn out to be able to capture accurately the development of the tip vortex. The simulations have also highlighted the influence of cavitation on the tip vortex trajectory.

Informations complémentaires


Jean Decaix


Decaix J.

Nom du congrès, lieu, date

9th International Symposium on Cavitation, EPFL, Lausanne, Switzerland, du 06.12.2015 au 10.12.2015