FINITE ELEMENT ANALYSIS OF SPECIMEN GEOMETRY EFFECTS ON FATIGUE CRACK CLOSURE

R. Craig McClung

Fatigue & Fracture of Engineering Materials & Structures · 1994 · 101 citations · 12 references

Concepts

Abstract

Abstract— Elastic‐plastic finite element analysis is used to study fatigue crack closure at three different crack length to width ratios for three plane stress specimen geometries: center‐cracked plate, single‐edge‐cracked plate (tension), and single‐edge‐cracked plate (bend). The maximum stress to flow stress ratio, S max /σ O , which successfully describes closure results in many center‐cracked plate configurations, does not correlate the effect of different geometries on the normalized opening stress, S open / S max . Crack opening stresses for different geometries and crack lengths are successfully correlated by a normalized stress intensity parameter, K max / K 0 , where K 0 =σ 0 φa. The quality of the correlation is very high at small K max / K 0 , and gradually deteriorates as K max / K 0 increases beyond the small‐scale yielding regime.

References

12