Derivation of 'γ' parameter form limit load expression of cracked component to evaluate J-R curve

摘要

Experimental evaluation of the J-integral requires the 'η{sub}(pl)' function, proposed by Rice et al. [Progress in flaw growth and fracture toughness testing (1973) 2311, to multiply the area under the load vs. plastic load-line-displacement curve. However, the J-integral, thus evaluated, requires modification if crack growth occurs. A 'γ' term was proposed by Hutchinson and Paris [Elastic-plastic fracture (1979) 37] and later generalised by Ernst et al. [Fracture mechanics (1979) 5811 and Ernst and Paris [Techniques of analysis of load-displacement records by J-integral methods (1980)] to correct the J-integral to account for crack growth. The η{sub}(pl) and γ functions are available for very few geometries under specific loading conditions. A limit load-based general expression of η{sub}(pl) was given by Roos et al. [Int J Pres Ves Piping 23 (1986) 81), but no such expression is available for γ functions. The advantage of having limit load-based general expressions for η{sub}(pl) and γ functions is that the limit load for a particular geometry subjected to a specific loading condition is easily available in the open literature. In the present paper, a limit load-based general expression for the γ function is derived. The general expression is then validated by deriving the known γ functions of various geometries subjected to various loading conditions, which are available in the open literature. The general expressions are then used to derive new η{sub}(pl) and 250L?functions for same pipe and elbow geometries with various crack configurations under different loading conditions, for which no solutions are available in the open literature. Finally, experiments have been carried out on 200 mm nominal bore (NB) elbows with throughwall circumferential cracks under in-plane bending moment. The proposed new expressions of η{sub}(p1) and γ functions for this geometry are used to obtain the J-R curve from the experimental load vs. load-line-displacement and load vs. crack growth data.