An analytical model for predicting residual stress in TBC-film cooling system considering non-uniform temperature field
Author:
Affiliation:
1. College of Power Engineering, Naval University of Engineering, Wuhan 430033, People’s Republic of China
Funder
National Major Science and Technology Projects of China
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0045148
Reference34 articles.
1. Thermal Barrier Coatings for Gas-Turbine Engine Applications
2. Thermal barrier coatings for aircraft engines: history and directions
3. Measurement of residual stress in thermal barrier coating using GIXRD
4. Thermal-barrier coatings for more efficient gas-turbine engines
5. An analytical model for predicting residual stresses in progressively deposited coatings Part 1: Planar geometry
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