Fatigue Crack Paths 2003
where multiplier it can be specified from the consistency condition of (9), F = 0, and
5 is a scalar measure of displacement discontinuity. Assumingthe critical stress value to
decrease with 5, a full decohesion, G6 = 0, occurs at 5 = 5c. The cohesive crack model
predicts the generation and growth of the damage zone governed by the cohesive law
(76 = (76(0) and also growth of crack occurring at 5= 5c. The application of the cohesive
crack modelto study growth of fatigue crack was presented by de Andre's et al. [14].
The concept of non-local description of crack initiation and propagation is natural
whena heterogeneous material structure is considered with randomly varying stress and
strain. The non-local values on any physical plane can be specified as follows
G.
i. <12) 1' r where Sr represents the averaging area and ar(r), r = ]x — y , is the weighting function which decreases with the distance r from the point x. The simplest case is when on, = 1 within the specified domain of size 06r and vanishes outside. Then Eq. (14) provide the meanvalues of stresses within specified plane domains. The formulation of Seweryn and Mroz [1, 2] followed the idea of non-local stress or strain measures on the critical plane area of size do >< d0. Denoting the resulting shear stress in the plane by 13, so that r..=]1]=(1ni2+1.22f (13> T h elocal failure functiontakes the f o r m 6 n I n Rf‘, = R6[ (l4) 7 6 C T C where (7c and to are the failure stresses in tension and shear. Analogously to the analysis of the strength of cracked body considering the microcrack opening and contact with accompanying slip and friction cf. Mroz and Seweryn [15], the elliptic condition for on 2 ]t'n]tang0d and the Coulomb condition for on < ]t'n]tangod was assumed (Fig. 1), thus 0,5 2 2 a t n + ” , on 2 ]tn]tang0d TBA (15) L 6 C R 0 ‘= [irni + G n t a ' n ( q+) fg o d)1: 6 n< ‘Tnita'ngod T C where (0d and (of denotes the dilatancy angle and the friction angle respectively.
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