Title of article :
Free-edge stresses and progressive cracking in surface coatings of circular torsion bars
Author/Authors :
Xiang-Fa Wu ، نويسنده , , Yuris A. Dzenis، نويسنده , , Kyle W. Strabala، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2008
Pages :
14
From page :
2251
To page :
2264
Abstract :
This paper considers the explicit solutions of free-edge stresses near circumferential cracks in surface coatings of circular torsion bars and their application in determining the progressive cracking density in the coating layers. The problem was formulated within the framework of linear elastic fracture mechanics (LEFM). The free-edge stresses near crack tip and the shear stresses in the cross-section of the torsion bar were approached in explicit forms based on the variational principle of complementary strain energy. Criterion for progressive cracking in the coating layer was established in sense of strain energy conservation, and the crack density is thereby estimated. Effects of external torque, aspect ratio, and elastic properties on the density of progressive cracking were examined numerically. The present study shows that, in the sense of inducing a given crack density, compliant coating layer with lower modulus has much higher critical torque than that of a stiffer one with the same geometries and substrate material, i.e., compliant coating layer has greater cracking tolerance. Meanwhile, the study also indicates that thicker surface coating layer is more pliant to cracking than the thinner ones. The present model can be used for analyzing the damage mechanism and cracking tolerance of surface coatings of torsion shafts and for data reduction of torsional fracture test of brittle surface coatings, etc.
Keywords :
Free-edge stress , Progressive cracking , Torsional shaft bar , Fracture criterion , Energy release rate (ERR , surface coatings
Journal title :
International Journal of Solids and Structures
Serial Year :
2008
Journal title :
International Journal of Solids and Structures
Record number :
449512
Link To Document :
بازگشت