Comparative Study on Different Methods for Prediction of Thermal Insulation Performance of Thermal Barrier Coating Used on Turbine Blades
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s11630-023-1904-x.pdf
Reference34 articles.
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3. Rao Y., Liu Y., Wan C., Multiple-jet impingement heat transfer in double-wall cooling structures with pin fins and effusion holes. International Journal of Thermal Sciences, 2018, 133: 106–119.
4. Zhang H., Zou Z., Li Y., et al., Conjugate heat transfer investigations of turbine vane based on transition models. Chinese Journal of Aeronautics, 2013, 26(4): 890–897.
5. Wang P., Li Y., Zou Z., et al., Conjugate heat transfer investigation of cooled turbine using the preconditioned density-based algorithm. Propulsion and Power Research, 2013, 2(1): 56–69.
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