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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

Study on full-coverage film cooling on center cone at engine-realistic conditions

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Pages 355-376 | Received 29 Apr 2022, Accepted 18 Jul 2022, Published online: 11 Aug 2022

References

  • J. A. Lovett, T. P. Brogan, D. S. Philippona, B. V. Keil and T. V. Thompson, “Development needs for advanced afterburner designs,” 40th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit. Florida, USA. Paper No. AIAA 2004-4192, 2004. DOI: 10.2514/6.2004-4192.
  • Y. K. Huang, X. M. He, Y. Jin, H. Y. Zhu and Z. X. Zhu, “Effect of non-uniform inlet profile on the combustion performance of an afterburner with bluff body,” Energy, vol. 216, pp. 119142–1-10, 2021. DOI: 10.1016/j.energy.2020.119142.
  • X. Z. Jia, Y. Shan, X. M. Tan and J. Z. Zhang, “Numerical investigation of effects of cooling structure parameters on performance of flameholder in an integrated afterburner,” Aerospace Sci. Technol., vol. 121, pp. 107378–1-12, 2022. DOI: 10.1016/j.ast.2022.107378.
  • Y. Q. Chen, Y. X. Fan and Q. X. Han, “Influence of cooling air jets on the aerodynamic and aerothermal losses and cooling effectiveness of air-cooled radial flameholder,” Int. J. Therm. Sci., vol. 172, pp. 107355–1-14, 2022. DOI: 10.1016/j.ijthermalsci.2021.107355.
  • X. Z. Jia, Y. Shan, X. P. Xu, J. Z. Zhang and X. M. Tan, “Effects of Bypass Flow Distribution on Cold Flow Characteristics of Integrated Afterburner,” Energies, vol. 14, no. 18, pp. 5842–1-10, 2021. DOI: 10.3390/en14185842.
  • J. Z. Zhang, S. C. Zhang, C. H. Wang and X. M. Tan, “Recent advances in film cooling enhancement: A review,” Chinese J. Aeronautics, vol. 33, pp. 1119–1136, 2020. DOI: 10.1016/j.cja.2019.12.023.
  • R. S. Bunker, “A review of turbine shaped film cooling technology,” ASME J. Heat Transfer, vol. 127, no. 4, pp. 441–453, 2005. DOI: 10.1115/1.1860562.
  • 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.
  • K. Singh, B. Premachandran and M. R. Ravi, “Experimental and numerical studies on film cooling of a corrugated surface,” Appl. Therm. Eng., vol. 108, pp. 312–329, 2016. DOI: 10.1016/j.applthermaleng.2016.07.093.
  • S. W. Lee, J. S. Lee and S. T. Ro, “Experimental study on the flow characteristics of streamwise inclined jets in crossflow on flat plate,” J. Turbomach., vol. 116, no. 1, pp. 97–105, 1994. DOI: 10.1115/1.2928283.
  • K. M. B. Gustafsson and T. G. Johansson, “An experimental study of surface temperature distribution on effusion-cooled plates,” J. Eng. Gas Turbines Power, vol. 123, no. 2, pp. 308–308, 2001. DOI: 10.1115/1.1364496.
  • S. K. Waye, “Film cooling effectiveness of suction side axial holes, compound angle holes, and axial holes embedded within an overlying transverse trench,” Master thesis, The University of Texas, Austin, USA, 2005.
  • J. J. Niu, C. L. Liu, H. Y. Liu, X. Xiao and J. F. Lin, “Theoretical and experimental analysis of overall cooling effectiveness for afterburner double-wall heat shield,” Int. J. Heat Mass Transfer, vol. 176, pp. 121360–1-12, 2021. DOI: 10.1016/j.ijheatmasstransfer.2021.121360.
  • W. Jessen, M. Konopka and W. Schroeder, “Particle-image velocimetry measurements of film cooling in an adverse pressure gradient flow,” ASME J. Turbomach., vol. 134, no. 2, pp. 021025–1-13, 2012. DOI: 10.1115/1.4003175.
  • M. Konopka, W. Jessen, M. Meinke and W. Schroeder, “Large-eddy simulation of film cooling in an adverse pressure gradient flow,” ASME J. Turbomach., vol. 135, no. 3, pp. 031031–1-13, 2013. DOI: 10.1115/1.4007583.
  • P. Ligrani et al., “Double wall cooling of a full coverage effusion plate with cross flow supply cooling and main flow pressure gradient,” J. Eng. Gas Turbines Power, vol. 141, no. 3, pp. 031015–1-11, 2019. DOI: 10.1115/1.4041451.
  • B. Zhang, H. H. Ji and Z. B. Zhang, “Numerical investigation of nozzle cavities thermal radiation characteristics with center cone cooled,” J. Aerospace Power, vol. 27, no. 3, pp. 50–565, 2012.
  • X. Wang, J. Z. Zhang and Y. Shan, “Effects of film hole arrangement on central-cone cooling and infrared radiation characteristics of exhaust system,” J. Aerospace Power, vol. 31, no. 4, pp. 830–835, 2016.
  • Y. Shan, J. Z. Zhang and W. R. Shao, “Experiments on aerodynamic and infrared radiation characteristics of film-cooling center-body exhaust system for a turbofan engine,” J. Aerospace Power, vol. 27, no. 1, pp. 9–15, 2012.
  • M. B. Gerdroodbary, M. Imani and D. D. Ganji, “Investigation of film cooling on nose cone by a forward facing array of micro-jets in hypersonic flow,” Int. Commun. Heat Mass Transfer, vol. 64, pp. 42–49, 2015. DOI: 10.1016/j.icheatmasstransfer.2015.02.015.
  • R. J. Moffat, “Describing the uncertainties in experimental results,” Exp. Therm. Fluid Sci., vol. 1, no. 1, pp. 3–17, 1988. DOI: 10.1016/0894-1777(88)90043-X.
  • R. Krewinkel, “A review of gas turbine effusion cooling studies,” Int. J. Heat Mass Transfer, vol. 66, pp. 706–722, 2013. DOI: 10.1016/j.ijheatmasstransfer.2013.07.071.
  • J. Z. Zhang, H. Xie and C. F. Yang, “Numerical study of flow and heat transfer characteristics of impingement/effusion cooling,” Chinese J. Aeronautics, vol. 22, no. 4, pp. 343–348, 2009. DOI: 10.1016/S1000-9361(08)60109-0.
  • Y. Wei-hua, C. Jun, S. Rui, H. Xu-Sheng and S. Shuang-wen, “Experimental investigation on impingement-effusion film-cooling behaviors in curve section,” Acta Astronautica, vol. 68, no. 11-12, pp. 1782–1789, 2011. DOI: 10.1016/j.actaastro.2011.02.001.
  • X. M. Tan, J. Z. Zhang and H. S. Xu, “Experimental investigation on impingement/effusion cooling with short normal injection holes,” Int. Commun. Heat Mass Transfer, vol. 69, pp. 1–10, 2015. DOI:10.1016/j.icheatmasstransfer.2015.09.005.

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