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Numerical Heat Transfer, Part A: Applications
An International Journal of Computation and Methodology
Volume 84, 2023 - Issue 4
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Research Articles

Effects of the multicavity tip coolant injection on the blade tip and the over tip casing aerothermal performance in a high-pressure turbine cascade

ORCID Icon, , , , & ORCID Icon
Pages 340-354 | Received 27 Apr 2022, Accepted 18 Jul 2022, Published online: 03 Aug 2022

References

  • R. S. Bunker, “A review of turbine blade tip heat transfer,” Ann. N. Y. Acad. Sci., vol. 934, pp. 64–79, 2001. DOI: 10.1111/j.1749-6632.2001.tb05843.x.
  • J. D. Denton, “Loss mechanisms in turbomachines,” ASME J. Turbomach., vol. 115, no. 4, pp. 621–656, 1993. DOI: 10.1115/1.2929299.
  • K. Du, L. Song, J. Li, and B. Sunden, “Effects of the layout of film holes near the vane leading edge on the endwall cooling and phantom cooling of the vane suction side surface,” Numer. Heat Transf. A: Appl., vol. 71, no. 9, pp. 910–927, 2017. DOI: 10.1080/10407782.2017.1326788.
  • K. Du, Z. Li, J. Li, and B. Sunden, “Influence of the pressure side injection slot on the cooling performance of endwall surface,” Numer. Heat Transf. A: Appl., vol. 73, no. 8, pp. 517–534, 2018. DOI: 10.1080/10407782.2018.1459140.
  • R. S. Bunker, “Axial turbine blade tips: Function, design, and durability,” AIAA J. Propuls. Power, vol. 22, no. 2, pp. 271–285, 2006. DOI: 10.2514/1.11818.
  • B. Sunden and G. Xie, “Gas turbine blade tip heat transfer and cooling: A literature survey,” Heat Transf. Eng., vol. 31, no. 7, pp. 527–554, 2010. DOI: 10.1080/01457630903425320.
  • N. L. Key and T. Arts, “Comparison of turbine tip leakage flow for flat tip and squealer tip geometries at high-speed conditions,” J. Turbomach., vol. 128, no. 2, pp. 213–249, 2006. DOI: 10.1115/1.2162183.
  • J. S. Kwak et al., “Heat transfer coefficients on the squealer tip and near tip regions a gas turbine blade with single or double squealer,” J. Turbomach., vol. 125, no. 4, pp. 778–787, 2003. DOI: 10.1115/1.1626684.
  • J. S. Kwak, J. Ahn, and J. C. Han, “Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade,” Int. J. Heat Mass Transf., vol. 47, no. 26, pp. 5651–5663, 2004. DOI: 10.1016/j.ijheatmasstransfer.2004.07.029.
  • D. Yang and Z. Feng, “Tip leakage flow and heat transfer predictions for turbine blades,” ASME Turbo Expo 2007: Power for Land, Sea, and Air. Montreal, Canada: American Society of Mechanical Engineers, 2007, pp. 589–596. DOI: 10.1115/GT2007-27728.
  • C. Zhou and H. Hodson, “Squealer geometry effects on aerothermal performance of tip-leakage flow of cavity tips,” J. Propuls. Power, vol. 28, no. 3, pp. 556–567, 2012. DOI: 10.2514/1.B34254.
  • J. Li, K. Du, and L. Song, “Effects of tip cavity geometries on the aerothermal performance of the transonic turbine blade with cavity tip,” Proceedings of the Institution of Mechanical Engineers Part a Journal of Power & Energy, London, UK, 2016.
  • N. Lamkin, A. Granovskiy, V. Belkanov, and J. Szwedowicz, “Effect of common blade tip squealer designs in terms of tip clearance loss control,” Proceedings of ASME 2013 Turbine Blade Tip Symposium & Course Week, TBTS2013-2040, Hamburg, Germany, 2013. DOI: 10.1115/TBTS2013-2040.
  • J. S. Park, S. H. Lee, J. S. Kwak, W. S. Lee, and J. T. Chung, “Measurement of blade tip heat transfer and leakage flow in a turbine cascade with a multi-cavity squealer tip,” ASME Turbine Blade Tip Symposium, Hamburg, Germany, 2013. DOI: 10.1115/TBTS2013-2072.
  • K. Du, Z. Li, J. Li, and B. Sunden, “Influences of a multi-cavity tip on the blade tip and the over tip casing aerothermal performance in a high-pressure turbine cascade,” Appl. Therm. Eng., vol. 147, pp. 347–360, 2019. DOI: 10.1016/j.applthermaleng.2018.10.093.
  • V. Shyam and A. Ameri, “Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating,” Vancouver, British Columbia, Canada, ASME, 2011. Paper No. GT2011-46390. DOI: 10.1115/GT2011-46390.
  • Q. Zhang and L. He, “Tip-shaping for HP turbine blade aerothermal performance management,” J. Turbomach., vol. 135, no. 5, pp. 051025, 2013.
  • C. Zhou, H. Hodson, I. Tibbott, and M. Stokes, “Effects of endwall motion on the aero-thermal performance of a winglet tip in a HP turbine,” J. Turbomach., vol. 134, no. 6, pp. 061036, 2012. DOI: 10.1115/1.4006302.
  • A. K. Saha, S. Acharya, R. Bunker, and C. Prakash, “Blade tip leakage flow and heat transfer with pressure-side winglet,” Int. J. Rotating Mach., vol. 2006, pp. 1–15, 2006. DOI: 10.1155/IJRM/2006/17079.
  • Z. Zou, F. Shao, Y. Li, W. Zhang, and A. Berglund, “Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance,” Energy, vol. 138, pp. 167–184, 2017. DOI: 10.1016/j.energy.2017.07.047.
  • Z. Zou, L. Xuan, Y. Chen, and F. Shao, “Effects of flow structure on heat transfer of squealer tip in a turbine rotor blade,” Int. Commun. Heat Mass Transf., vol. 114, pp. 104588, 2020. DOI: 10.1016/j.icheatmasstransfer.2020.104588.
  • K. Huang, J. Zhang, C. Wang, and S. Liu, “Large-eddy simulation of single-row serrated trenched-hole film cooling on turbine guide vane,” Int. Commun. Heat Mass Transf., pp. 1–23, 2022.
  • R. J. Goldstein, “Film cooling,” Adv. Heat Transf., vol. 7, pp. 321–380, 1971.
  • D. G. Bogard and K. A. Thole, “Gas turbine film cooling,” J. Propuls. Power, vol. 22, no. 2, pp. 249–270, 2006. DOI: 10.2514/1.18034.
  • R. S. Bunker, “A review of shaped hole turbine film-cooling technology,” J. Heat Transfer Trans. ASME, vol. 127, no. 4, pp. 441–453, 2005. DOI: 10.1115/1.1860562.
  • J. C. Han, S. Dutta, and S. V. Ekkad, Gas Turbine Heat Transfer and Cooling Technology, New York: Taylor & Francis, 2000.
  • J. C. Han, “Advanced cooling in gas turbines - 2016 Max Jakob memorial award paper,” J. Heat Transf., vol. 140, no. 11, pp. 113001, 2018.
  • J. S. Kwak and J. C. Han, “Heat transfer coefficient and film cooling effectiveness on the squealer tip of a gas turbine blade,” ASME J. Turbomach., vol. 125, no. 4, pp. 648–657, 2003. DOI: 10.1115/1.1622712.
  • S. P. Mhetras, D. Narzary, Z. Gao, and J. C. Han, “Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip,” ASME J. Turbomach., vol. 130, no. 2, pp. 021002, 2008.