Conjugate Heat Transfer Predictions on Combined Impingement and Film Cooling of a Blade Leading Edge Model

References

• M. V. Jensen and J. H. Walther, “Numerical analysis of jet impingement heat transfer at high jet Reynolds number and large temperature difference,” Heat Transf. Eng., vol. 34, no. 10, pp. 801–809, 2013. DOI: 10.1080/01457632.2012.746153.
   Web of Science ®Google Scholar
• K. Chen, P. X. Jiang, J. N. Chen, and R. N. Xu, “Numerical investigation of jet impingement cooling of a flat plate with carbon dioxide at supercritical pressures,” Heat Transf. Eng., vol. 39, no. 2, pp. 85–97, 2018. DOI: 10.1080/01457632.2017.1288042.
   Web of Science ®Google Scholar
• B. R. Hollworth and L. Dagan, “Arrays of impingement jets with spent fluid removal through vent holes on the target surface, part I: average heat transfer,” J. Eng. Gas Turbines Power, vol. 102, no. 4, pp. 994–999, 1980. DOI: 10.1115/1.3230372.
   Web of Science ®Google Scholar
• S. V. Ekkad, Y. Huang, and J. C. Han, “Impingement heat transfer on a target plate with film holes,” J. Thermophys. Heat Transfer, vol. 13, no. 4, pp. 522–528, 1999. DOI: 10.2514/2.6471.
   Web of Science ®Google Scholar
• D. E. Metzger and R. S. Bunker, “Local heat transfer in internally cooled turbine airfoil leading edge regions: Part II—impingement cooling with film coolant extraction,” J. Turbomach., vol. 112, no. 3, pp. 459–466, 1990. DOI: 10.1115/1.2927681.
   Web of Science ®Google Scholar
• M. E. Taslim, Y. Pan, and S. D. Spring, “An experimental study of impingement on roughened airfoil leading-edge walls with film holes,” J. Turbomach., vol. 123, no. 4, pp. 766–773, 2001. DOI: 10.1115/1.1401035.
   Web of Science ®Google Scholar
• M. E. Taslim, Y. Pan, and K. Bakhtari, “Experimental racetrack shaped jet impingement on roughened leading edge wall with film holes,” presented at the Proceedings of ASME Turbo Expo 2002: Power for Land, Sea, and Air, Amsterdam, The Netherlands, GT2002-30477, Jun. 3–6, 2002, pp. 897–906. DOI: 10.1115/GT2002-30477.
   Google Scholar
• M. E. Taslim and A. Khanicheh, “Experimental and numerical study of impingement on an airfoil leading edge with and without showerhead and gill film holes,” J. Turbomach., vol. 128, no. 2, pp. 310–320, 2006. DOI: 10.1115/1.2137742.
   Web of Science ®Google Scholar
• B. D. Mouzon, E. J. Terrel, J. E. Albert, and D. G. Bogard, “Net heat flux reduction and overall effectiveness for a turbine blade leading edge,” presented at the Proceedings of ASME Turbo Expo 2004: Power for Land, Sea, and Air, Reno, NV, USA, GT2005-69002, Jun. 6–9, 2005, pp. 825–832. DOI: 10.1115/GT2005-69002.
   Google Scholar
• L. D. Dobrowolski, D. G. Bogard, J. Piggush, and A. Kohli, “Numerical simulation of a simulated film cooled turbine blade leading edge including conjugate heat transfer effects,” presented at the ASME 2009 International Mechanical Engineering Congress and Exposition, Lake Buena Vista, FL, USA, IMECE2009-11670, Nov. 13–19, 2009, pp. 2145–2156. DOI: 10.1115/IMECE2009-11670.
   Google Scholar
• S. Ravelli, L. Dobrowolski, and D. G. Bogard, “Evaluating the effects of internal impingement cooling on a film cooled turbine blade leading edge,” presented at the Proceedings of ASME Turbo Expo 2010: Power for Land, Sea, and Air, Glasgow, UK, GT2010-23002, Jun. 14–18, 2010, pp. 1655–1665. DOI: 10.1115/GT2010-23002.
   Google Scholar
• J. Maikell, D. B. Bogard, J. Piggush, and A. Kohli, “Experimental simulation of a film cooled turbine blade leading edge including thermal barrier coating effects,” J. Turbomach., vol. 133, no. 1, pp. 011014, 2011. DOI: 10.1115/1.4000537.
   Web of Science ®Google Scholar
• S. Mathew, S. Ravelli, and D. G. Bogard, “Evaluation of CFD predictions using thermal field measurements on a simulated film cooled turbine blade leading edge,” J. Turbomach., vol. 135, no. 1, pp. 011021, 2013. DOI: 10.1115/1.4006397.
   Web of Science ®Google Scholar
• T. E. Dyson, D. G. Bogard, J. D. Piggush, and A. Kohli, “Overall effectiveness for a film cooled turbine blade leading edge with varying hole pitch,” J. Turbomach., vol. 135, no. 3, pp. 31011, 2013. DOI: 10.1115/1.4006872.
   Web of Science ®Google Scholar
• T. E. Dyson, D. G. Bogard, and S. D. Bradshaw, “Evaluation of CFD simulations of film cooling performance on a turbine vane including conjugate heat transfer effects,” Int. J. Heat Fluid Flow, vol. 50, pp. 279–286, Dec. 2014. DOI: 10.1016/j.ijheatfluidflow.2014.08.010.
   Web of Science ®Google Scholar
• M. L. Nathan, T. E. Dyson, D. G. Bogard, and S. D. Bradshaw, “Adiabatic and overall effectiveness for the showerhead film cooling of a turbine vane,” J. Turbomach., vol. 136, no. 5, pp. 031005, 2014. DOI: 10.1115/1.4024680.
   Web of Science ®Google Scholar
• W. R. Stewart and D. G. Bogard, “Experimental thermal field measurements of film cooling above the suction surface of a turbine vane,” J. Eng. Gas Turbines Power, vol. 137, no. 10, pp. 102604, 2015. DOI: 10.1115/1.4030263.
   Web of Science ®Google Scholar
• K. Chavez, T. N. Slavens, and D. G. Bogard, “Effects of internal and film cooling on the overall effectiveness of a fully cooled turbine airfoil with shaped holes,” presented at the Proceedings of ASME Turbo Expo 2016: Power for Land, Sea, and Air, Seoul, South Korea, GT2016-57992, Jun. 13–17, 2016. DOI: 10.1115/GT2016-57992.
   Google Scholar
• J. Wang, K. Tian, H. Zhu, M. Zeng, and B. Sundén, “Numerical investigation of particle deposition in film-cooled blade leading edge,” Num. Heat Transf. A Appl., vol. 77, no. 6, pp. 579–598, 2020. DOI: 10.1080/10407782.2020.1713692.
   Web of Science ®Google Scholar
• S. J. Li, S. F. Yang, and J. C. Han, “Effect of coolant density on leading edge showerhead film cooling using the pressure sensitive paint measurement technique,” J. Turbomach., vol. 136, no. 5, 051011, 2014. DOI: 10.1115/1.4025225.
   Web of Science ®Google Scholar
• S. B. Islami, S. P. A. Tabrizi, B. A. Jubran, and E. Esmaeilzadeh, “Influence of trenched shaped holes on turbine blade leading edge film cooling,” Heat Transf. Eng., vol. 31, no. 10, pp. 889–906, 2010. DOI: 10.1080/01457630903550317.
   Web of Science ®Google Scholar
• W. D. York and J. H. Leylek, “Leading-edge film-cooling physics—Part III: diffused hole effectiveness,” J. Turbomach., vol. 125, no. 2, pp. 252–259, 2003. DOI: 10.1115/1.1559899.
   Web of Science ®Google Scholar
• G. G. Barigozzi and S. S. Ravelli, “Combined experimental and numerical study of showerhead film cooling in a linear nozzle vane cascade,” presented at the Proceedings of ASME Turbo Expo 2015: Power for Land, Sea, and Air, Montreal, QC, Canada, GT2015-42397, Jun. 15–19, 2015, DOI: 10.1115/GT2015-42397.
   Google Scholar
• Z. Liu, L. Ye, C. Y. Wang, and Z. P. Feng, “Numerical simulation on impingement and film composite cooling of blade leading edge model for gas turbine,” Appl. Therm. Eng., vol. 73, no. 2, pp. 1432–1443, 2014. DOI: 10.1016/j.applthermaleng.2014.05.060.
   Web of Science ®Google Scholar
• Z. Liu, L. Ye, and Z. P. Feng, “Numerical study of impingement and film composite cooling on blade leading edge,” presented at the Proceedings of ASME Turbo Expo 2014: Power for Land, Sea, and Air, Dusseldorf, Germany, GT2014-26643, Jun. 16–20, 2014. DOI: 10.1115/GT2014-26643.
   Google Scholar
• L. P. Timoko, “Energy efficient engine high pressure turbine component test performance report,” National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH, USA, Tech. Rep. NASA-CR-168289, 1984.
   Google Scholar
• X. Yang et al., “Experimental and numerical investigations of overall cooling effectiveness on a vane endwall with jet impingement and film cooling,” Appl. Therm. Eng., vol. 148, pp. 1148–1163, Feb. 2019. DOI: 10.1016/j.applthermaleng.2018.11.116.
   Web of Science ®Google Scholar