Issue 32
I. Telichev, Frattura ed Integrità Strutturale, 32 (2015) 24-34; DOI: 10.3221/IGF-ESIS.32.03 30 Using the expansion of the function u 2 (ξ) in terms of Lagrange interpolation polynomials over the Chebyshev’s nodes we obtain the expression for the function * * 2 2 ( ) g x : * 2 1 1 * * * 2 2 2 2 2 1 1 1 1 ( ) (1) 1 2 1 N N k r k r k r x g x g u T T d N (6) After integration * 2 1 * 2 2 1 x d arccos x and * 2 1 * 2 2 1 1 r x T d sin r arccos x r we get 1 * * * * * 2 2 2 2 2 2 1 1 1 1 ( ) (1) 2 N N k r k k r g x g u arccos x T sin r arccos x N r (7) Analogously we obtain the expressions for * * 0 0 ( ) g x and * * 1 1 ( ) g x at * 0 0 0 0 0 / , x x l x L and * 1 1 1 1 1 / , x x l x L : 1 * * * * * 0 0 0 0 0 0 0 0 0 0 0 1 1 1 1 ( ) (1) / 2 N N k r k k r g x g g x g l l u arccos x T sin r arccos x N r (8) * * * 1 1 1 1 1 1 1 1 ( ) (1) / g x g g x g l l 1 * * 1 1 1 1 1 1 1 2 N N k r k k r u arccos x T sin r arccos x N r (9) From Eq. (2) in the symmetric case we have ' ' ' ' 1 æ v v v 4 g x x x x G (10) Integrating we obtain the relation: (1 ) ( ) v v v( ) 2 4 n n æ g x x C G , where n is a segment number. The constants of integration C n are determined by displacement at the end of the segment: 2 0 C 2 2 1 (1 ) 4 æ g l C G 1 1 0 1 1 1 2 2 (1 ) (1 ) 4 4 æ g l æ C C g l g l G G Thus the crack opening displacement (COD) for the segment L n is defined as following * * * * (1 ) ( ) ( ) 2v( ) 2 2 n n n n n n æ l g x COD x x C G (11) Since for the plane stress (1 ) 2 4 æ G E , the expression for * ( ) n COD x takes the form 1 * * * 1 1 4 1 ( ) 2 [ 2 ] , 0,1,2 N N n k n Y n n n r k n k r Y u l S COD x C arccos x T sin r arccos x n EN S r (12)
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