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 RANS 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.


Published in:
9Th International Symposium On Cavitation (Cav2015), 656, 012183
Presented at:
9th International Symposium on Cavitation (CAV), Ecole Polytechnique Federale Lausanne, Lausanne, SWITZERLAND, DEC 06-10, 2015
Year:
2015
Publisher:
Bristol, Iop Publishing Ltd
ISSN:
1742-6588
Laboratories:




 Record created 2016-02-16, last modified 2018-03-17


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