Crack Shapes and Stress Intensity Factors for Edge-Cracked Specimens
- 1 January 1972
- book chapter
- Published by ASTM International
Abstract
A simple stress intensity factor expression is given for a deep edge crack in a plate in tension. The shapes of cracks opened by tension or bending are approximated by conic sections and the conic section coefficients related to plate geometry by very simple empirical equations. The magnitude of the crack displacement is a function of applied load, plate geometry, and the elastic constants of the plate material. The shape of a loaded crack in a semi-infinite plate is, approximately, a portion of an ellipse whose semimajor axis is about three times the crack length. As the crack length (relative to the plate width) increases, the crack shape becomes parabolic, then hyperbolic, the acuity of the hyperbola increasing with the relative crack length.This publication has 5 references indexed in Scilit:
- Stress intensity factors for deep cracks in bending and compact tension specimensEngineering Fracture Mechanics, 1970
- Elastic displacements for various edge-cracked plate specimensInternational Journal of Fracture, 1968
- Discussion: “Analysis of Stresses and Strains Near the End of a Crack Traversing a Plate” (Irwin, G. R., 1957, ASME J. Appl. Mech., 24, pp. 361–364)Journal of Applied Mechanics, 1958
- Analysis of Stresses and Strains Near the End of a Crack Traversing a PlateJournal of Applied Mechanics, 1957
- Stress distribution in a notched plateMathematika, 1957