2019
DOI: 10.1016/j.ijmultiphaseflow.2019.04.003
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Slug-to-churn vertical two-phase flow regime transition study using an interface tracking approach

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Cited by 28 publications
(10 citation statements)
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“…The adaptive mesh refinement capabilities used in PHASTA were also verified and it was shown to successfully capture wavy interface structures of annular flow as well as reduce the computational costs (Rodriguez et al, 2013). More recently, a slug-to-churn flow regime transition study reported favorable agreement between PHASTA results and the existing experimental and analytical results for complex two-phase flow regimes (Zimmer and Bolotnov, 2019). The two-phase flow simulation capability can also be extended to even larger engineering problems, such as nuclear reactor subchannels (Fang et al, 2017(Fang et al, , 2018(Fang et al, , 2020.…”
Section: Flow Solver and Interface Capturing Approachmentioning
confidence: 81%
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“…The adaptive mesh refinement capabilities used in PHASTA were also verified and it was shown to successfully capture wavy interface structures of annular flow as well as reduce the computational costs (Rodriguez et al, 2013). More recently, a slug-to-churn flow regime transition study reported favorable agreement between PHASTA results and the existing experimental and analytical results for complex two-phase flow regimes (Zimmer and Bolotnov, 2019). The two-phase flow simulation capability can also be extended to even larger engineering problems, such as nuclear reactor subchannels (Fang et al, 2017(Fang et al, , 2018(Fang et al, , 2020.…”
Section: Flow Solver and Interface Capturing Approachmentioning
confidence: 81%
“…Severe deformation may result in bubble break-up, which leads to more complex flow regimes. One such example is the slug bubble during the slug-to-churn flow regime transition (Zimmer and Bolotnov, 2019). As the gas flow rate increases, satellite bubbles are teared off from the slug bubble which contribute to the interface instability and eventually trigger the transition.…”
Section: Introductionmentioning
confidence: 99%
“…The largest loss of void is observed in mesh 9-10, although the difference is rather small with mesh 10-10 and 10-11. Quite interestingly, the average shape of the bubble tail varies from flat (9-10) to somewhat concave (10-10) and somewhat convex (10)(11). The streamlines indicate that the bubble itself consists of a large toroidal vortex with its rotational center relatively close to the tail.…”
Section: Simulation Strategy Meshing and Averagingmentioning
confidence: 98%
“…However, a deviation of the turbulent fluctuations in the wake of the Taylor bubble due to over-prediction of the loss of void of the Taylor bubble made the authors of [2] conclude that the LES mesh resolution is not sufficient to capture the break-up and bubble formation accurately. Meanwhile, other researchers have also performed high fidelity simulation of turbulent Taylor bubble flow, e.g., see [10] and [11].…”
Section: Introductionmentioning
confidence: 99%
“…The rapid advent of high-performance computing (HPC) systems has only recently enabled excursions into large-scale interface-resolved simulations of complex two-phase flows. Using the strongly parallel scaled, finite-element-method-based code-PHASTA (Parallel Hierarchic Adaptive Stabilized Transient Analysis) [28,29]-and the level-set interface capturing method [30], two-phase simulations have been performed for conditions representative of PWR flow regimes, including bubbly flows [31][32][33], slug-to-churn flow [34] and the DFFB regime [35] (from our prior work). Interface tracking method [36] and immersed boundary method [37] have also been used for simulating bubbly flows; however, their challenging numerical implementation precludes applicability to complex geometries and complex interface topologies.…”
Section: Introductionmentioning
confidence: 99%