This paper presents the implementation and assessment of a modified Partially averaged Navier-Stokes (PANS) turbulence model which can successfully predict the transient cavitating turbulent flows. The proposed model treats the standard k-epsilon model as the parent model, and its main distinctive features are to (1) formulate the unresolved-to-total kinetic energy ratio (f (k) ) based on the local grid size as well as turbulence length scale, and (2) vary the f (k) -field both in space and time. Numerical simulation used the modified PANS model for the sheet/cloud cavitating flows around a three-dimensional Clark-Y hydrofoil. The available experimental data and calculations of the standard k-epsilon model, the f (k) = 0.8 PANS model, the f (k) = 0.5 PANS model are also provided for comparisons. The results show that the modified PANS model accurately captures the transient cavitation features as observed in experiments, namely, the attached sheet cavity grows in the flow direction until to a maximum length and then it breaks into a highly turbulent cloud cavity with three-dimensional structures in nature. Time-averaged drag/lift coefficients together with the streamwise velocity profiles predicted by the proposed model are in good agreement with the experimental data, and improvements are shown when compared with results of the standard k-epsilon model, the f (k) = 0.8 PANS model and the f (k) = 0.5 PANS model. Overall, the modified PANS model shows its encouraging capability of predicting the transient cavitating turbulent flows.
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IIT Madras, Dept Mech Engn, Chennai 600036, Tamil Nadu, India
IIT Kharagpur, Dept Ocean Engn, Kharagpur, W Bengal, IndiaIIT Madras, Dept Mech Engn, Chennai 600036, Tamil Nadu, India
Chakraborty, Arnab
Warrior, H., V
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IIT Kharagpur, Dept Ocean Engn, Kharagpur, W Bengal, IndiaIIT Madras, Dept Mech Engn, Chennai 600036, Tamil Nadu, India
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Jiangsu Univ, Natl Res Ctr Pumps, Zhenjiang 212013, Jiangsu, Peoples R China
Univ Padua, Dept Ind Engn, I-35121 Padua, Veneto, Italy
UNIPD, Turbomachinery & Energy Syst Grp, Padua, ItalyJiangsu Univ, Natl Res Ctr Pumps, Zhenjiang 212013, Jiangsu, Peoples R China
Yin, Tingyun
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Pavesi, Giorgio
Pei, Ji
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Jiangsu Univ, Natl Res Ctr Pumps, Zhenjiang 212013, Jiangsu, Peoples R ChinaJiangsu Univ, Natl Res Ctr Pumps, Zhenjiang 212013, Jiangsu, Peoples R China
Pei, Ji
Yuan, Shouqi
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Jiangsu Univ, Natl Res Ctr Pumps, Zhenjiang 212013, Jiangsu, Peoples R ChinaJiangsu Univ, Natl Res Ctr Pumps, Zhenjiang 212013, Jiangsu, Peoples R China
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School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing,100191, ChinaSchool of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing,100191, China
Luo, Da-Hai
Yan, Chao
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School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing,100191, ChinaSchool of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing,100191, China
Yan, Chao
Wang, Xiao-Yong
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School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing,100191, ChinaSchool of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing,100191, China