2001
DOI: 10.1016/s0376-0421(01)00014-8
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Dynamics of attached turbulent cavitating flows

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Cited by 270 publications
(164 citation statements)
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“…The following general lognormal distribution can be applied to approximately describe the nucleus-size spectral distribution [113]: 15) where Σ, ψ and ξ are fitting parameters, which depend on the considered fluid (ξ and Σ represent the average radius and the standard deviation of the distribution, respectively). Each nucleus evolves according to the Rayleigh-Plesset equation, that is, the radius (R 0 ) of the considered nucleus is used as the initial condition to solve equation (5.9).…”
Section: (A) the Rayleigh-plesset Equation For Single-bubble Dynamicsmentioning
confidence: 99%
“…The following general lognormal distribution can be applied to approximately describe the nucleus-size spectral distribution [113]: 15) where Σ, ψ and ξ are fitting parameters, which depend on the considered fluid (ξ and Σ represent the average radius and the standard deviation of the distribution, respectively). Each nucleus evolves according to the Rayleigh-Plesset equation, that is, the radius (R 0 ) of the considered nucleus is used as the initial condition to solve equation (5.9).…”
Section: (A) the Rayleigh-plesset Equation For Single-bubble Dynamicsmentioning
confidence: 99%
“…Model boundary condition has been formulated as follows [18,[20][21][22]: • constant and uniform velocity v in profile in the inlet cross-section, simultaneously local level of k, and ∈ indirectly by setting turbulence intensity ε and characteristic length scale λ 2 in…”
Section: General Concept and Computational Model Of Cavitating Devicementioning
confidence: 99%
“…Wang et al [14] performed a series of experiments to study time-dependent cavitating flows around a Clark-Y hydrofoil. Figure 1 shows the shapes of cavities during an oscillation cycle.…”
Section: Evaluation Of Transport Equation-based Models (Tem)mentioning
confidence: 99%
“…The capability for simulating unsteady cavitating flows with the different cavitation models is further investigated. The computational domain and boundary conditions are given according to the experimental setup [14], which is shown in Figure 2. The Clark-Y hydrofoil is located at the center of the test section with the angle of attack equal to 8°.…”
Section: Evaluation Of Transport Equation-based Models (Tem)mentioning
confidence: 99%