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15 3. Flows through stationary ribbed passages. 2-Dimensional Flows P/e =10 e/D=0.0675 P/e=10 e/H=0.1

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3. Flows through stationary ribbedpassages.

2-Dimensional Flows

P/e =10e/D=0.0675

P/e=10e/H=0.1

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Ribbed Channel

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Comparisons with non-linear k- ��

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3-Dimensional Flows

Flow Details

Body-fitted grid

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Nusselt Number Comparisons for HeatedDuct with Staggered Ribs

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Flow in a Ribbed U-Bend

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Flow in a Duct with Inclined Ribs

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Heat Transfer in a Duct with Inclined Ribs

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Comments

� In two-dimensional flows through ribbedchannels and pipes

- Zonal Models under-predict Nusselt number- Low-Re Models predict the right Nusselt

number levels- Second-Moment closured produced the Nu

variation more faithfully- The initial form of the Differential Yap term

too strong for the second-moment closure.- The recent version of the non-linear k- �

produced satisfactory predictions.

� In three-dimensional flows through ducts andU-bends with normal ribs.

- Mean flow development predicted well byall models.

- Turbulence field better predicted by second-moment closures.

- Heat transfer comparisons lead to similarconclusions as for 2-D flows.

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� In ducts with inclined ribs

- Flow field well predicted by zonal models

- Nusselt number distribution and levels alsowell predicted by zonal models.

- Rib induced secondary motion makes theheat transfer predictions less sensitive to themodeling of the near-wall turbulence.

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4. Flows through rotating ribbed passages.

Rotating Duct With Normal Ribs

Mean Flow Comparisons

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Rotating Duct With Normal Ribs

Comparisons of Turbulent Stresses

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Flow in a Rotating Duct With Inclined RibsPredicted Effect of Rotation on Mean Motion.

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Flow in a Rotating Duct With Inclined RibsMean Flow Comparisons

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Heat Transfer in a Rotating Duct WithInclined RibsNu Contours

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Heat Transfer in a Rotating Duct WithInclined Ribs

Side-Averaged Nusselt Number

____ : 2-Layer DSM ------ : 2-Layer k- �

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Comments

� Rotation is shown to have a noticeable effect onthe mean and turbulent flow fields.

� All models tested able to reproduce the meanflow correctly.

� Effects of rotation on turbulence better capturedby the second-moment closures.

� As also found under stationary conditions, inpassages with inclined ribs, 2- layer (zonal)models produce reasonable heat transferpredictions.

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5. Concluding Remarks

�In many heat convection problems inengineering applications, such as blade cooling,the flow is complex and three-dimensional.

�Flow features present can include

- Streamline Curvature- Secondary Motion- Flow Separation- Flow Impingement- Streamwise acceleration- Body forces such as the Coriolis and the

Centrifugal force.

�This pauses severe challenges to currentlyavailable turbulence models, especially whenit comes to the prediction of the correct wallheat transfer.

In flows affected by streamline curvature andsecondary motion, is often advantageous tomove away from the conventional wall-functions and to also employ second-momentclosures.

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�Flow separation induced by strong curvature,is better predicted by second-moment closuresand also requires the use of high-orderdiscretization for all transport equations.

� Heat transfer in rotating passages with smoothsurfaces becomes especially difficult to predictwhen either rotational buoyancy becomessignificant, or when rotation is combined withstrong curvature.

For the prediction of heat transfer in passageswith normal ribs, low-Re models are essential.

�In inclined ribs, due to the presence ofsecondary motion, the thermal predictions of thezonal models are closer to the data.

�A differential length-scale correction (Yap)term, leads to further predictive improvements.

�Recently refined non-linear k- �� models offer analternative modelling route.

�Recent developments in wall-functions offerfurther possibilities.

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Bibliography

1. Iacovides H and Launder B EThe numerical simulation of flow and heat transfer in tubes in orthogonalmode rotation. Proc. 6th Int. Symp. on Turbulent Shear Flows, Toulouse, 1987.2. Iacovides H and Launder B EPrediction of turbulent flow and heat transfer in a 180-deg bend of squarecross-section.2nd National UK Heat Transfer Conference, Glasgow, 1988.3. Choi Y-D, Iacovides H and Launder B E.Numerical computation of turbulent flow in a square-sectioned 180-deg bend.ASME J Fluids Engrg, 111, pp 59-68, 1989.

4. Iacovides H and Launder B E.Parametric and numerical study of fully-developed flow and heat transfer inrotating rectangular ducts.ASME Int Gas-Turbine and Aero Congress, Brussels, 1990.Also ASME Journal of Turbomachinery, 113, pp 331-338, 1991.5. Bo T, Iacovides H and Launder B EConvective discretization schemes for the turbulence transport equations inflow predictions through sharp U-bends.Int. Journal of Numerical Methods in Heat and Fluid Flow, 5, pp 33-48,1995.6. Bo T, Iacovides H and Launder B E.Developing buoyancy-modified turbulent flow in ducts rotating in orthogonalmode.ASME Journal of Turbomachinery, 117,474-484, 1995.7. Iacovides H, Launder B E and Li H-Y The computation of flow development through stationary and rotating U-bends of strong curvature. Int Journal of Heat and Fluid Flow, 17,22-23,1995.8. Iacovides H. and Launder B EComputational fluid dynamics applied to internal cooling of gas-turbineblade cooling : a reviewInt of Journal Heat and Fluid Flow, 16 , 454-470,1995.

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9. Bo T and Iacovides HNumerical study of the effects of rotational buoyancy on fully developedflow in rotating rectangular ducts.Int. Journal of Num. Meth. for Heat and Fluid Flow, Vol 6, No 7, 47-62,1996.10. Iacovides H, Launder B E and Li H-Y. Application of a Reflection-Free DSM to Turbulent Flow and Heat Transferin a Square-Sectioned U-Bend.Int. Journal of Experimental Thermal and Fluid Science, 13, 419-429, 1996.11. H IacovidesComputation of flow and heat transfer through rotating ribbed passagesInternational Journal of Heat and Fluid Flow, 19, 393-400,1998.12. H. IacovidesThe computation of turbulent flow through stationary and rotating U-bendswith rib-roughened surfaces.International Journal for Numerical Methods in Fluids, 29, 865-876, 1999.13. H. Iacovides and M RaiseeRecent progress in the computation of flow and heat transfer in internalcooling passages of turbine blades.International Journal of Heat and Fluid Flow, 20,320-328,1999.14. Craft T J, Iacovides H and Yoon J HProgress in the use of non-linear two-equation models in the computation ofconvective heat-transfer in impinging and separated flows.Flow, Turbulence and Combustion, 63,59-80,1999.15. Iacovides H and Raisee M,Computation of Flow and Heat Transfer in Two-Dimensional Rib-Roughened Passages,using low-Reynolds-number turbulence models. Int J. Numerical Methods Heat and Fluid Flow, Vol 11, No 2, pp 138-155,200116. H. Iacovides, G. Kelemenis and M. RaiseeOn the Effects of inclines Ribs on the Flow and Thermal Development inStraight Cooling Passages; An Experimental and Computational StudyJournal of.Expt Thermal and Fluid Science, Vol 27,Issue 3, pp 283-294,200317. Y. Okita, and H. IacovidesComparison of EVM and DSM in Flow and Heat Transfer of Turbine Blades Internal CoolingPassages with a Wall Function Method, Acepted, ASME Journal of Turbomachinery, 2003.18. H. Iacovides and M. RaiseeTurbulent Flow and Heat Transfer in Stationary and Rotating Cooling Passages with Inclined

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Ribs on Opposite Walls.Paper GT-2004-53245, ASME IGTI International Gas-Turbine and Aero Congress, Vienna2004.19. M Raisee, A Noursadeghi and H. IacovidesPrediction of Convective Heat Transfer Through Ribbed Channels Using a Lowe-Re Non-Linear k-� Model. Int. Journal for Numerical Methods in Heat and Fluid Flow, 14, No 3, p285-304, 200420. K-P S Nikas and H IacovidesThe Computation of flow and heat transfer through square-ended U-bends , using Low-Reynolds-number models.Int. Journal for Numerical Methods in Heat and Fluid Flow, 14, No 3, p 305-324, 200421. K-S P. Nikas and H. IacovidesThe Computation of Flow and Heat Transfer Through an Orthogonally Rotating Square-EndedU-Bend, Using Low-Reynolds-Number Models.To Appear, International Journal of Rotating Machinery, 2004.22. M Raisee, H. Alemi and H IacovidesPrediction of Developing Turbulent Flow in a 90o curved duct, using linear and non-linear low-Re k-� models.Paper ESDA2004-58466, 7th Biennial ASME Conference on Engineering Design andAnalysis, Manchester, UK, 2004