Abstract

When the width of cracked nanocomponents made of brittle or quasi-brittle materials is less than approximately , the size of the - dominance zone becomes smaller than and comparable to the fracture process zone ( ). The fracture process starts to be dominated by far-stress field terms and the critical stress intensity factor can no more represent the total fracture driving force. This means a breakdown of a classical linear elastic fracture mechanics suffering from the undesirable crack-tip stress singularity. The contribution presents a new concept expected to properly predict the critical crack driving force for nano-components: The ab-initio aided strain gradient elasticity theory (AI-SGET). In contrast to the Barenblatt cohesive model, the strain gradient elasticity theory does not require to prescribe a suitable field of cohesive tractions along the crack faces in order to eliminate the stress singularity and to exhibit cusp-like profiles of crack flanks close to the crack front in accordance with atomistic models. The only unknown and necessary quantity is the material length scale parameter which can be, e.g., determined by best strain gradient elasticity fits of ab-initio computed phonon-dispersions and near-dislocation displacement fields. Atomistic approaches can also be employed to determine fracture mechanical parameters (crack driving force, crack tip opening displacement) related to the moment of crack instability in a given material. Such AI-SGET codes can then be utilized to a successful prediction of fracture of cracked nanocomponents made of brittle or quasi-brittle materials.

Highlights

  • The basic hypothesis of linear fracture mechanics says that the size of the K - dominant region must be much higher than the fracture process zone incorporating inelastic deformations near the crack-tip

  • The finite element (FE) model of a center cracked nano-panel consisting of a tungsten with elastic coefficients of the cubic structure c11 = 523GPa, c12 = 205 GPa and c44 = 161 GPa is introduced as the numerical example to illustrate the cohesion relation at the crack tip

  • Detailed FE calculations of the cracked nanopanel subjected to mod I loading in terms of the SGET were carried out under the plane strain conditions

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Summary

Introduction

The basic hypothesis of linear fracture mechanics says that the size of the K - dominant region must be much higher than the fracture process zone incorporating inelastic deformations near the crack-tip. Strain gradient elasticity; Ab-initio adjustment; Stress singularity; Cusp-like crack profile; Cracked nanopanel. In contrast to the Barenblatt cohesive model, the strain gradient elasticity theory does not require to prescribe a suitable field of cohesive tractions along the crack faces in order to eliminate the undesirable stress singularity and to produce cusp-like profiles of near-tip crack faces in accordance with atomistic models even when the simplest form of the SGET is used containing elastic constants and one length material parameter only.

Results
Conclusion

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