Abstract
2D-finite element model for analysis of thermal and stress-strain state of ceramic thermal barrier coatings (TBC) on the cooled turbine blades allowing for the creep deformation in blade and coating is described. Coating life is estimated according to the criterion of exhaustion of ceramic coating adhesive strength.
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© 1991 Elsevier Science Publishers Ltd
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Tamarin, Y.A., Soundyrin, V.G., Kanayev, V.Y. (1991). Stress Calculation the Ceramic Thermal Barrier Coatings for the Cooled Turbine Blades. In: Cocks, A.C.F., Ponter, A.R.S. (eds) Mechanics of Creep Brittle Materials 2. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-3688-4_26
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DOI: https://doi.org/10.1007/978-94-011-3688-4_26
Publisher Name: Springer, Dordrecht
Print ISBN: 978-1-85166-701-7
Online ISBN: 978-94-011-3688-4
eBook Packages: Springer Book Archive