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A numerical evaluation on the effect of sister holes on film cooling effectiveness and the surrounding flow field

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Abstract

A numerical study was performed to evaluate the effectiveness of the novel sister hole film cooling technique. Two secondary coolant holes bound the primary coolant hole slightly downstream of its midpoint, intended to minimize the primary vortex pair and improve cooling performance. An unstructured hexahedral mesh was generated and the realizable kε turbulence model with near-wall modeling was used in these simulations. Blowing ratios of 0.2, 0.5, 1.0, and 1.5 were simulated to evaluate the applicability of sister holes in practical applications. It was found that sister holes significantly improved cooling performance over the entire computational domain, particularly at high blowing ratios. These results arose by countering the primary vortex pair with a secondary pair from these sister holes, ultimately maintaining flow adhesion where the coolant stream would have otherwise separated.

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Abbreviations

A :

Area

D :

Diameter

DR:

Density ratio

L :

Length

M :

Blowing ratio

Ma :

Mach number

P :

Perimeter

R :

Gas constant

T :

Temperature

V :

Velocity

h :

Height

k :

Turbulent kinetic energy

p :

Pitch

s :

Row spacing

y + :

The normalized distance yu */v

z :

Coordinate in the lateral direction

ε:

Dissipation rate of turbulent kinetic energy

η:

Adiabatic effectiveness

μ:

Viscosity

ρ:

Density

ν:

Eddy viscosity

aw:

Adiabatic wall

c:

Coolant

h:

Hydraulic

t:

Turbulent

w:

Wetted

∞:

Freestream

References

  1. Bogard D, Thole K (2006) Gas turbine film cooling. J Propuls Power 22:249–270

    Article  Google Scholar 

  2. Sargison J, Oldfield M, Guo S, Lock G, Rawlinson A (2005) Flow visualizations of the external flow from a converging slot-hole film cooling geometry. Exp Fluids 38:304–318

    Article  Google Scholar 

  3. Baheri S, Alavi-Tabrizi SP, Jubran BA (2007) Film cooling effectiveness from trenched shaped and compound holes. Heat Mass Transf 44:989–998

    Article  Google Scholar 

  4. Yuen C, Martinez-Botas R (2003) Film cooling characteristics of a single round hole at various streamwise angles in a crossflow: part I effectiveness. Heat Mass Transf 46:221–235

    Article  Google Scholar 

  5. Azzi A, Jubran BA (2003) Numerical modeling of film cooling from short length stream-wise injection holes. Heat Mass Transf 39:344–353

    Google Scholar 

  6. Bergeles G, Gosman AD, Launder BE (1978) The turbulent jet in a cross stream at low injection rates: a three-dimensional numerical treatment. Num Heat Transf 1:217–242

    Google Scholar 

  7. Roy S (2000) Numerical investigation of the blade cooling effect generated by multiple jets issuing at an angle into an incompressible horizontal crossflow. Num Heat Transf Part A 28:701–718

    Article  Google Scholar 

  8. Javadi A, Javadi K, Taeibi-Rahni M, Darbandi A (2003) A new approach to improve film cooling effectiveness using combined jets. In: Proceedings of the international conference on gas turbine cong 2003, paper # TS-071, Tokyo, Japan

  9. Javadi K, Taeibi-Rahni M, Darbandi M (2007) Jet-into-crossflow boundary-layer control: innovation in gas turbine blade cooling. AIAA J 25:2910–2925

    Article  Google Scholar 

  10. Heidmann D (2008) A numerical study of anti-vortex film cooling designs at high blowing ratio. Proc ASME Turbo Expo 2008, GT2008-50845

  11. Dhungel A (2007) Film cooling from a row of holes supplemented with anti-vortex holes. Master’s thesis, Louisiana State University, Baton Rouge, LA

  12. Kusterer K, Bohn D, Sugimoto T, Tanaka R (2007) Double-jet ejection of cooling air for improved film cooling. J Turbomach 29:809–815

    Article  Google Scholar 

  13. Kusterer K, Bohn D, Sugimoto T (2008) Double-jet film-cooling for highly efficient film-cooling with low blowing ratios. Proc ASME Turbo Expo 2008, GT2008-50073

  14. Ajersch P, Zhou J, Ketler S, Salcudean M, Gartshore I (1997) Multiple jets in a crossflow: detailed measurements and numerical simulations. J Turbomach 119:330–342

    Article  Google Scholar 

  15. Harrison, K, Bogard, D (2008) Comparison of RANS turbulence models for prediction of film cooling performance, ASME Turbo Expo 2008, GT2008-51423

  16. Ely M, Jubran BA (2008) A numerical study on improving film cooling performance through the use of sister holes. Proc ASME Turbo Expo 2008, GT2008-50366

  17. Goldstein R, Eckert E, Burggraf F (1974) Effects of hole geometry and density on three-dimensional film cooling. Heat Mass Transf 17:595–607

    Article  Google Scholar 

  18. Gartshore I, Salcudean M, Hassan I (2001) Film cooling injection hole geometry: hole shape comparison for compound cooling orientation. AIAA J 39:1493–1499

    Article  Google Scholar 

  19. Yavuzkurt S, Habte M (2008) Effect of computational grid on performance of two-equation models of turbulence for film cooling applications, ASME Turbo Expo 2008, GT2008-50153

  20. Shih T, Liou W, Shabbir A, Yang Z, Zhu J (1995) A new kε eddy-viscosity model for high Reynolds number turbulent flows—model development and validation. Comp Fluids 24:227–238

    Article  MATH  Google Scholar 

  21. Inc FLUENT (2003) Fluent 6.1 users guide. FLUENT Inc., Lebanon, NH

    Google Scholar 

  22. Sinha A, Bogard D, Crawford N (1991) Film cooling effectiveness downstream of a single row of holes with variable density ratio. J Turbomach 113:442–449

    Article  Google Scholar 

  23. Na S, Shih T (2007) Increasing adiabatic film-cooling effectiveness by using an upstream ramp. J Heat Transf 129:464–471

    Article  Google Scholar 

Download references

Acknowledgments

The authors would like to extend their thanks to the Natural Science and Engineering Research Council of Canada and the Province of Ontario for their funding towards this research. Special thanks are also due to the High Performance Computing Virtual Laboratory for their financial support and extensive resources.

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Correspondence to Marc J. Ely.

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Ely, M.J., Jubran, B.A. A numerical evaluation on the effect of sister holes on film cooling effectiveness and the surrounding flow field. Heat Mass Transfer 45, 1435–1446 (2009). https://doi.org/10.1007/s00231-009-0523-8

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  • DOI: https://doi.org/10.1007/s00231-009-0523-8

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