Predicting turbulent flow in a staggered tube bundle

International Journal of Heat and Fluid Flow

Volumn 20, Issue 6, 1999, Pages 581-591

  Watterson, J K ^a   Dawes, W N ^b   Savill, A M ^b   White, A J ^b  

^a QUEEN'S UNIVERSITY BELFAST   (United Kingdom)

^b UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

CFD; Turbulence models; Unstructured meshes

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; INCOMPRESSIBLE FLOW; NAVIER-STOKES EQUATIONS; TURBULENT FLOW;

EID: 0033400771     PISSN: 0142727X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-727X(99)00049-1     Document Type: Article

References (19)

1. Dawes W.N. The practical application of solution-adaption to the numerical solution of complex turbomachinery problems. Progress in Aerospace Sciences. 29:1993;221-269.
2. Hanjalic, K., Hadzic, I., 1998. 3rd ERCOFTAC-IAHR workshop on refined flow modelling: turbulent flow and heat transfer in a sub-channel of a staggered tube bundle. T.U. Delft Technical Report.
3. Harlow F.H., Amsden A.A. A numerical fluid dynamics calculation method for all flow speeds. J. Comp. Phys. 8:1971;197-213.
4. Issa R.I., Lockwood F.C. On the prediction of two-dimensional supersonic viscous interactions near walls. AIAA J. 15(2):1977;182-188.
5. Jameson, A., Baker, T.J., 1987. Improvements to the aircraft Euler method. In: AIAA 25th Aerospace Science Meeting, Paper 87-0452.
6. Kim J., Moin P., Moser R. Turbulent statistics in fully developed channel flow at low reynolds number. J. Fluid Mech. 177:1987;133-166.
7. Leschziner, M. A., Launder, B. E., 1993. Round normally impinging turbulent jet and turbulent flow through tube bank sub-channel. In: Proceedings of 2nd ERCOFTAC-IAHR workshop on refined flow modelling, UMIST.
8. Mavriplis D.J. Accurate multigrid solution of the euler equations on unstructured and adaptive meshes. AIAA J. 28(2):1990;213-221.
9. Mavriplis, D.J., Jameson, A., Martinelli, L., 1989. Multigrid solution of the Navier-Stokes equations on triangular meshes. NASA CR-181786, ICASE Rep. No. 89-11.
10. McGuirk J.J., Page G.J. Shock capturing using a pressure-correction method. AIAA J. 28(10):1990;1751-1757.
11. Ng, Y.-K., 1992. A high-resolution coupled parabolic/elliptic Navier-Stokes solver for turbomachinery flows. Ph.D. thesis, Whittle Laboratory, University of Cambridge.
12. Patankar S.V. Numerical Heat Transfer and Fluid Flow. 1980;Hemisphere, Washington, DC.
13. Shyy W., Chen M.-H., Sun C-S. Pressure-based multigrid algorithm for flow at all speeds. AIAA J. 30(11):1992;2660-2669.
14. Simonin, D., Barcouda, M., 1988. Measurements and predictions of turbulent flow entering a staggered tube bundle. EDF report H-44/88.25.
15. Thomas, J.L., Walters, R.W., Reu, T., Ghaffari, F., Weston, R.P., Luckring, J.M., 1989. A patched-grid algorithm for complex configurations directed towards the F-18 Aircraft. AIAA 27th Aerospace Science Meeting Paper 89-0121.
16. Watterson, J.K., 1994. A pressure-based flow solver for the three-dimensional Navier-Stokes equations on unstructured and adaptive meshes. In: 25th AIAA Fluid Dynamics Conference, Paper 94-2358.
17. Watterson, J.K., Dawes, W.N., Savill, A.M., White, A.J., 1994. Turbulent flow in a staggered bundle of cylinders without heat transfer. In: 3rd ERCOFTAC-IAHR Workshop on Refined Flow Modelling, Lisbon.
18. Watterson J.K., Connell I.J., Savill A.M., Dawes W.N. A solution adaptive mesh procedure for predicting confined explosions. Int. J. Numer. Meth. Fluids. 26:1998;235-247.
19. Yang, Z., Shih, T.H., 1993. A k-ε model for turbulent and transitional boundary layers. In: So, R.M.C., Speziale, C.G., Launder, B.M. (Eds.), Near Wall Turbulent Flows. Elsevier, Amsterdam, pp. 165-176.