journal article·2008-05

Analysis of crack nets development in thermal barrier coatings

Asher A. Rubinstein, Yaliang Tang

International Journal of Fracture· Volume 151· Issue 1
Publisher page

Abstract

After a relatively short time in service, components with thermal barrier coatings (TBCs) protection typically develop a system of cracks that propagate from the coated surface toward the interface. Usually these cracks propagate across the thickness of the protective coating and branch along the interface between the coating and the bank metal. The presence of these crack nets is a concern for the durability of the components with TBCs. In the study of thin TBCs by Rubinstein and Tang (Int J Solids Struct 42:5831–5847, 2005), it was found that in a number of cases, these components may still serve for a long time because of crack growth resistance development for cracks growing along the interface, which was found to be the most stable crack path under thermal loading conditions. One of the aims of this study is to determine whether similar fracture resistance is typical for thick TBC coatings as well. The emphases of the analysis presented here are on cases when the coating thickness is comparable to the thickness of the bank material, and on the effect of heat conduction changes due to branching of the developing cracks in a direction parallel to or along the interface. These items were not addressed in sufficient detail in the previous investigations.
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Research context

OpenAlex topics: Materials Engineering and Processing · Material Properties and Applications · Material Properties and Failure Mechanisms

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References (18)

Show source-provided references
1. Evans AG, He MY, Hutchinson JW (2001) Mechanics-based scaling laws for the durability of thermal barrier coatings. Prog Mater Sci 46:249–271 doi: 10.1016/S0079-6425(00)00007-410.1016/S0079-6425(00)00007-4 ↗
2. Hsueh CH (2002) Thermal stresses in elastic multilayer system. Thin Solid Films 418:182–188 doi: 10.1016/S0040-6090(02)00699-510.1016/S0040-6090(02)00699-5 ↗
3. Hutchinson JW, Lu TJ (1995) Laminate delamination due to thermal gradients. J Eng Mater Technol 117:386–390 doi: 10.1115/1.280473010.1115/1.2804730 ↗
4. Hutchinson JW, Suo Z (1992) Mixed mode cracking in layered materials. Adv Appl Mech 29:63–19110.1016/S0065-2156(08)70164-9 ↗
5. Kakac S, Yener Y (1985) Heat conduction, 2nd edn. Hemispher Publishing Company
6. Lee Y, Erdogan F (1998) Interface cracking of FGM coatings under steady state heat flow. Eng Fract Mech 59(3):361–380 doi: 10.1016/S0013-7944(97)00137-910.1016/S0013-7944(97)00137-9 ↗
7. Qian G, Nakamura T, Berndt CC (1998) Effects of thermal gradient and residual stress on thermal barrier coating fracture. Mech Mater 27:91–110 doi: 10.1016/S0167-6636(97)00042-210.1016/S0167-6636(97)00042-2 ↗
8. Rice JR, Sih GC (1965) Plane problems of cracks in dissimilar media. J Appl Mech 32:418–42310.1115/1.3625816 ↗
9. Rizk AA, Erdogan F (1989) Cracking of coated materials under transient thermal stresses. J Therm Stresses 12:125–168 doi: 10.1080/0149573890896195910.1080/01495738908961959 ↗
10. Rubinstein AA (1986) Macrocrack–microdefect interaction. J Appl Mech Trans ASME 53:505–51010.1115/1.3171803 ↗
11. Rubinstein AA (1991) Mechanics of a crack path formation. Int J Fract 47:291–305 doi: 10.1007/BF0001294810.1007/BF00012948 ↗
12. Rubinstein AA, Choi HC (1988) Macrocrack interaction with a transverse array of parallel microcracks. Int J Fract 36:15–2610.1007/BF00034814 ↗
13. Rubinstein AA, Tang Y (2005) Micromechancal analysis of failure in thin protective coatings. Int J Solids Struct 42:5831–5847 doi: 10.1016/j.ijsolstr.2005.03.02410.1016/j.ijsolstr.2005.03.024 ↗
14. Shulze GW, Erdogan F (1998) Periodic cracking of elastic coatings. Int J Solids Struct 35:3615–3634 doi: 10.1016/S0020-7683(97)00228-X10.1016/S0020-7683(97)00228-X ↗
15. Zhu D, Miller RA (1998a) Influence of high cycle thermal loads on thermal fatigue behavior of thick thermal barrier coatings. NASA technical report, NASA TP-3676, pp 3–10
16. Zhu D, Miller RA (1998b) Investigation of thermal high cycle and low cycle fatigue mechanisms of thick thermal barrier coatings. NASA/TM-1998-20663310.1016/S0921-5093(97)00852-6 ↗
17. Zhu D, Miller RA (1998) Investigation of thermal high cycle and lower fatigue mechanism of thick thermal barrier coatings. Mater Sci Eng A 245:212–22310.1016/S0921-5093(97)00852-6 ↗
18. Zhu D, Ghosn LJ, Miller RA (1998) Effect of layer-graded bond coats on edge stress concentrations and oxidation behavior of thermal barrier coatings. NASA/TM-1998-208505