Record number :
1689402
Title of article :
Simulation of crack propagation in thermal barrier coatings with friction
Author/Authors :
Bنker، نويسنده , , Martin and Rِsler، نويسنده , , Joachim، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2012
Pages :
4
From page :
236
To page :
239
Abstract :
Thermal barrier coatings, frequently used in turbine blades, comprise a corrosion-protecting bond coat, a ceramic top coat and a growing oxide layer in between. Failure mechanisms of these coating systems are still not satisfactorily understood. In this paper, crack initiation in thermal barrier coatings is studied with two-dimensional finite element simulations. It is assumed that the crack direction of a propagating crack is determined by a maximum energy release rate. Trial cracks are used to find the optimum propagation direction. It is shown that radial stresses near the peak position of the rough interface are compressive so that cracks propagating parallel to the interface are loaded mainly in mode II. Friction on the crack surface can be easily taken into account with the trial crack method. It is shown that cracks tend to kink away from the interface and that this tendency is more pronounced when friction is present. The influence of creep on the energy release rate is also studied. Creep relaxation strongly reduces the stresses and the energy release rates and can be approximately accounted for by a simple estimate.
Keywords :
Thermal barrier coatings , Finite element method , crack propagation , Interface , Energy Release
Journal title :
Computational Materials Science
Journal title :
Computational Materials Science
Serial Year :
2012
Link To Document :
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