Numerical Analysis of Multi-zone Trench Cooling on an Adiabatic Flat Plate for Gas Turbine Application
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-67241-5_29
Reference12 articles.
1. Broomfield, R.W., Ford, D.A., Bhangu, H.K., Thomas, M.C., Frasier, D.J., Burkholder, P.S., Wahl, J.B.: Development and turbine engine performance of three advanced rhenium containing superalloys for single crystal and directionally solidified blades and vanes. In Turbo Expo: Power for Land, Sea, and Air (Vol. 78712, p. V004T12A001). American Society of Mechanical Engineers. (1997) https://doi.org/10.1115/97-GT-117
2. Mishra, M.P., Sahani, A.K., Chandel, S., Mishra, R.K.: Enhancement of full coverage film cooling effectiveness with mixed injection holes. Int. J. Turbo & Jet-Engines (2018). https://doi.org/10.1515/tjj-2018-0025
3. Hou, R., Wen, F., Luo, Y., Tang, X., Wang, S.: Large eddy simulation of film cooling flow from round and trenched holes. Int. J. Heat Mass Transf. 144, 118631 (2019). https://doi.org/10.1016/j.ijheatmasstransfer.2019.118631
4. Wang, C., Sun, X., Zhang, J.: Uncertainty analysis of trench film cooling on flat plate. Appl. Therm. Eng. 156, 562–575 (2019). https://doi.org/10.1016/j.applthermaleng.2019.04.099
5. Shi, B., Li, X., Ren, J.: Adiabatic effectiveness and heat transfer measurements of simple and trenched cylindrical holes with backward injection. Int. J. Therm. Sci. 170, 107086 (2021). https://doi.org/10.1016/j.ijthermalsci.2021.107086
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