journal article·2020-01

Stress analysis of the thermal barrier coating system near a cooling hole considering the free-edge effect

Jishen Jiang, Xianfeng Ma, Biao Wang

Ceramics International· Volume 46· Issue 1
Publisher page

Abstract

Abstract Due to the thermal mismatch between layers and the free-edge effect, interfacial peeling and shear stresses are generated locally around the edges of cooling holes in a thermal barrier coating (TBC)–film cooling system. These interfacial peeling and shear stresses may lead to modes I and II edge delamination, resulting in TBC spallation around the cooling hole. In this study, analytical and numerical models were built to study the stress and interfacial cracking behaviors of TBCs near the cooling hole. Analytical solutions for interfacial peeling moment and shear force at each layer were obtained to analyze the free-edge effect on the stress distributions in TBCs, and they were verified by the finite element calculations. The results showed that interfacial peeling moment and shear force were functions of the hole radius and thicknesses of top coat and oxide layer. The increase of interfacial peeling moment and shear force raised the likelihood of edge cracking around the hole. Derived by the local stresses, the interfacial cracks in TBCs initiated and propagated from the hole edge upon cooling.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: High-Temperature Coating Behaviors · Heat Transfer Mechanisms · Particle Dynamics in Fluid Flows

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (24)

Show source-provided references
1. Thermal barrier coatings for gas-turbine engine applications10.1126/science.1068609 ↗
2. Thermal-barrier coatings for more efficient gas-turbine engines10.1557/mrs.2012.232 ↗
3. Influence of material properties on temperature and thermal stress of thermal barrier coating near a normal cooling hole10.1016/j.ijheatmasstransfer.2011.08.026 ↗
4. Numerical stress analysis of the TBC-film cooling system under operating conditions considering the effects of thermal gradient and TGO growth10.1016/j.surfcoat.2018.10.020 ↗
5. Effects of surface deposition, hole blockage, and TBC spallation on vane endwall film-cooling
6. Sun · 2012
7. Deformation and cracking near a hole in an oxide-forming alloy foil subjected to thermal cycling10.1016/j.actamat.2012.09.077 ↗
8. The stress distribution around goles in thermal barrier coatings10.1016/j.msea.2004.03.062 ↗
9. Mechanisms controlling the durability of thermal barrier coatings10.1016/S0079-6425(00)00020-7 ↗
10. Thermal stresses in elastic multilayer systems10.1016/S0040-6090(02)00699-5 ↗
11. An analytical model for predicting thermal residual stresses in multilayer coating systems10.1016/j.tsf.2005.04.027 ↗
12. Edge effects in thin film delamination10.1016/S1359-6454(00)00293-7 ↗
13. Stresses in BiMetal thermostats10.1115/1.3176133 ↗
14. Realistic modeling of edge effect stresses in bimaterial elements10.1115/1.2904333 ↗
15. Interfacial shear and peel stresses in multilayered thin stacks subjected to uniform thermal loading10.1115/1.2905382 ↗
16. Estimation of transverse/interlaminar stresses in laminated composites–a selective review and survey of current developments10.1016/S0263-8223(99)00126-9 ↗
17. Thermomechanical peeling in multilayer beams and plates—a solution from first principles10.1016/j.ijsolstr.2004.07.013 ↗
18. Interfacial peeling moments and shear forces at free edges of multilayers subjected to thermal stresses10.1111/j.1551-2916.2006.00924.x ↗
19. Residual stresses in meta/ceramic bonded strips10.1111/j.1151-2916.1985.tb15316.x ↗
20. Timoshenko · 1959
21. Edge effect on crack patterns in thermally sprayed ceramic splats10.1007/s11666-016-0505-6 ↗
22. Numerical analyses of the residual stress and top coat cracking behavior in thermal barrier coatings under cyclic thermal loading10.1016/j.engfracmech.2018.04.031 ↗
23. Version ABAQUS. 6.13 · 2013
24. The free-edge stress singularity at an interface between bilinear materials10.1016/0020-7683(91)90050-P ↗