A Flux-Conservation Mixing Plane Algorithm for Multiphase Non-Equilibrium Steam Models
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The accuracy of steady multistage turbomachinery calculations is dependent on the exchange of information at an interface, also known as mixing plane, between adjacent blade rows. This paper describes an extension of already available flux conservation mixing plane algorithm to the Eulerian-Eulerian non-equilibrium steam model. Since algorithms that conserve fluxes across the interface have been found to be more accurate and robust, greater emphasis is on the conservation of mixture and droplet fluxes across the interface. The key characteristics of the algorithm are provided, along with its application on simple two- and three-dimensional blade rows.
2014 ◽
Vol 16
(27)
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pp. 13974-13983
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2021 ◽
Vol 2021.74
(0)
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pp. A41
2021 ◽
Vol 159
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pp. 106591
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2015 ◽
Vol 86
(12)
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pp. 1490-1497
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2020 ◽
Vol 153
◽
pp. 106348
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