Comparison of Two Two-Equation Turbulence Model Used for the Numerical Simulation of Underwater Ammunition Fuze Turbine Flow Field

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Abstract:

To figure out the problem of turbulence simulation of underwater ammunition fuze turbine numerical simulation, respectively, realizable k-ε turbulence model and SST k-ω turbulence model are used for two-phase flow numerical simulation of the turbine rotation. The analysis compared the calculation results of the two turbulence models. The results showed that: the cavitation scale obtained from realizable k-ε turbulence model is shorter than that of SST k-ω turbulence model; turbine surface pressure distribution trends are similar of this two model, the results of realizable k-ε turbulence model are bigger than SST k-ω turbulence model; the turbine axial pressure coefficients using realizable k-ε turbulence model are also bigger than that of SST k-ω turbulence model, and the deviation increases with the speed increase.

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Periodical:

Advanced Materials Research (Volumes 591-593)

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1968-1972

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November 2012

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] A.K. Singhal, M.M. Athavale. Journal of Fluids Engineering, Vol. 124(2002), p.617

Google Scholar

[2] J. Zhao, Y.J. Wei, J.Z. Zhang, L. Dong, D.Q. Jin. Engineering Mechanics, Vol. 26(2009) No.8, p.233. (In Chinese)

Google Scholar

[3] B. Huang, G.Y. Wang, X.B Quan, G.H. Chen. Chinese Journal of Applied Mechanics, Vol. 28( 2011) No.4, p.339 (In Chinese)

Google Scholar

[4] B. Huang, G.Y. Wang. China Mechanical Engineering. 21(1), 2010: 85-89 (In Chinese)

Google Scholar

[5] B. Zhang, G.Y. Wang, S.L. Zhang, Z.Y. Yu. Transactions of Beijing Institute of Technology, Vol. 28(2008) No.12, p.1065. (In Chinese)

Google Scholar

[6] T.H. shih, W.W. Liou, A. Shabbir, Z. G. Yang, J. Zhu. Compute Fluids. Vol. 24(1995) No.3, p.227

Google Scholar

[7] F.R. Menter. AIAA-93-2906, 1993.

Google Scholar

[8] C.J. Xu, H. Zhang. Journal of Projectiles, Rockets, Missiles and Guidance, Vol. 26(2006) No.1, p.110. (In Chinese)

Google Scholar