PSI - Issue 14
Filin V.Yu. et al. / Procedia Structural Integrity 14 (2019) 758–773 Author name / Structural Integrity Procedia 00 (2018) 000–000
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3
elastic modulus
E
total applied strain (service plus residual strain)
e
yield strain
e Y
function accounting for the decrease of residual stress under a high load
f 1 f 2
function correlating the values of J and J el
f R6 boundary function between the safe and unsafe areas of failure assessment diagram (FAD) G elastic energy release rate J J-integral J c critical value of J-integral, a parameter of material J el elastic part of J-integral K I stress intensity factor (SIF) under Mode I loading K Ia SIF at a crack arrest, a parameter of material K Ic critical SIF at Mode I loading, a parameter of material ( K c ) J critical SIF calculated via J-integral K r relative SIF l crack length along the surface L specimen span or parallel length L r relative load M load moment m coefficient accounting for stress-strain state n 1 reserve factor in strength condition in terms of J-integral n 3 reserve factor in “absolute” strength condition in terms of J-integral n case reserve factor exponent accounting for the design case n i number of valid test outcomes at one temperature NDT nil ductility temperature P load Q constraint parameter r distance from crack tip S full thickness of a structural element ds element of the contour t specimen thickness T temperature T d minimum design temperature T traction vector of the value on the contour defined in relation to an outward normal unit vector TKB ductile to cleavage transition temperature with big samples U elastic energy of the body u displacement vector V data variation coefficient v crack mouth opening displacement, CMOD v pl plastic part of CMOD W specimen width w strain energy density x distance ahead a crack tip in the crack plane
Y t , Y b dimensionless functions accounting for tension and bending Y r , Y a dimensionless functions for the examined flaw size and position
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