Effect of Inertia on Finite Near-Tip Deformation for Fast Mode-III Crack Growth.

Abstract

The combined effects of finite deformation and material inertia ave been analyzed for fast crack growth under anti-plane loading conditions. A steady-state dynamic solution has been obtained for the finite strain on the crackline, from the moving crack tip to the moving transition boundary with the z one of small strains. The crack propagates in a material with a response curve in uniform shear that is linear at small strains, and that remains constant once a critical strain has been exceeded. The corresponding quasi-static solution is given in the full zone of large deformation. For the dynamic formulation, an explicit expression for the crack-line strain has been obtained by expanding the displacement in a power series in the distance to the crackline, with coefficients which depend on the distance to the moving crack tip. Substitution in the equation of motion yields a nonlinear ordinary differential equation for the relevant coefficient, which can be solved rigorously. The finite deformation crack-line fields have been matched to appropriate small-strain fields at the transition boundary. The principal result is that the dynamic strain remains bounded at the crack tip, apparently due to the effect of material inertia.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1984
Accession Number
ADA142947

Entities

People

  • Jan D. Achenbach
  • Nobuhiko Nishimura

Organizations

  • Northwestern University

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Applied Mechanics
  • Boundaries
  • Cartesian Coordinates
  • Civil Engineering
  • Coefficients
  • Constitutive Equations
  • Continuity
  • Coordinate Systems
  • Crack Tips
  • Differential Equations
  • Equations
  • Materials
  • Mechanics
  • Military Research
  • Power Series
  • Steady State
  • Stresses

Readers

  • Fluid Dynamics.
  • Materials Science (Mechanical Engineering).