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Improvement of Film Cooling Performance of a Slot on a Flat Plate Using Coanda Effect

코안다 효과를 이용한 평판 슬롯의 막냉각 성능 향상

  • Kim, Gi Mun (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Kim, Ye Jee (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Kwak, Jae Su (School of Aerospace and Mechanical Engineering, Korea Aerospace University)
  • 김기문 (한국항공대학교 항공우주 및 기계공학부) ;
  • 김예지 (한국항공대학교 항공우주 및 기계공학부) ;
  • 곽재수 (한국항공대학교 항공우주 및 기계공학부)
  • Received : 2016.10.04
  • Accepted : 2016.11.10
  • Published : 2017.04.01

Abstract

In this study, the Coanda effect inducing bump was applied to improve the film cooling effectiveness on the flat plate with $30^{\circ}$ and $45^{\circ}$ angled rectangular slots. The slot length to width ratio was 6. A cylindrical cap shaped structure, called Coanda bump, was installed at the exit of the slot to generate Coanda effect. The width and height of the bump was 10.5 mm and 1 mm, respectively. The film cooling effectiveness was measured at the fixed blowing ratio, M=2.0, using pressure sensitive paint (PSP) technique. The mainstream velocity was 10 m/s and the turbulence intensity was about 0.5%. Results showed that the film cooling effectiveness for case of $30^{\circ}$ angled slot was higher than that of $45^{\circ}$ angled slot. It was found that there was no positive effect of Coanda effect on the overall averaged film cooling effectiveness for the $30^{\circ}$ angled slot. On the other hand, for the $45^{\circ}$ angled slot, the film cooling effectiveness was improved with the installation of the Coanda bump.

Keywords

References

  1. Goldstein, R. J., 1971, "Film Cooling," Advances in Heat Transfer, Vol. 7, pp. 321-379.
  2. Bogard, D. G., 2006, "Gas Turbine Film Cooling," AIAA Journal of Propulsion and Power, Vol. 22. No. 2.
  3. Wright, L. M., Gao, Z., Yang, H., and Han, J. C., 2006, "Film Cooling Effectiveness Distribution on a Gas Turbine Blade Platform with Inclined Slot Leakage and Discrete Film Hole Flows," ASME Turbo Expo, Barcelona, Spain, GT2006-90375.
  4. Papa, M., Srinivasan, V., and Goldstein, R. J., 2012, "Film Cooilng Effect of Rotor-Stator Purge Flow on Endwall Heat/Mass Trasfer," ASME Journal of Turbomachinery, Vol. 134.
  5. Abo El-Azm, M. M., Shalash, K. M., and El-Gabry, L. A., 2014, "INVESTIATION OF A NOVEL DISCRETE SLOT FILM COOLING SCHEME," ASME Turbo Expo, Dusseldorf, Germany, GT2014-26019.
  6. Sellars, N. D. and Wood, N. J. 2002, "DELTA WING CIRCULATION CONTROL USING THE COANDA EFFECT," AIAA Paper No. AIAA 2002-3269.
  7. FISER, J., JEDELSKY, J., VACHFORMAN, T., and JÍCHA, M., 2012, "COMPARISON OF CFD SIMULATIONS AND MEASUREMENTS OF FLOW AFFECTED BY COANDA EFFECT," EPJ Web of Conferences 25, 01015 (2012).
  8. Kim, H. D., Raghunathan, S., Setoguchi, T., and Matsuo, S., 2000, "EXPERIMENTAL AND NUMERICAL STUDIES OF SUPERSONIC COANDA WALL JETS," AIAA Paer No. AIAA 2000-0814.
  9. Transcossi, M., Dumas, A., Das, S. S., and Pascoa, J., 2014, "Design methods of Coanda effect nozzle with two streams," INCAS BULLETIN, Vol. 6, Issue 1/2014, pp. 8 3-95. https://doi.org/10.13111/2066-8201.2014.6.1.8
  10. Dumas, A., Subhash, M., Transcossi, M., and Marques, J. P., 2013, "The influence of surface temperature on Coanda effect," 68th Conference of the Italian Thermal Machines Engineering Association, AT2013.
  11. Benabed, M., 2015, "Computational Optimization of Coanda Effect on Film-Cooling Performance," J. Thermophysics and Heat Transfer, Vol. 29, Issue 4.
  12. Han, J. C. and Rallabandi, A. P., 2010, "Turbine Blade Film Cooling Using PSP Technique," Frontiers in Heat and Mass Transfer(FHMT), 1-013001.
  13. Charbonnier, D., Ott, P., Jonsson, M., Cottier, F., and Kobke, Th., 2009, "Experimental and Numerical Study of the Thermal Performance of a Film Cooled Turbine Platform," ASME Paper, GT2009-60306.