A specimen for a constant stress intensity factor
โ Scribed by J. Schuve; A.U. De Koning
- Publisher
- Elsevier Science
- Year
- 1977
- Tongue
- English
- Weight
- 699 KB
- Volume
- 9
- Category
- Article
- ISSN
- 0013-7944
No coin nor oath required. For personal study only.
โฆ Synopsis
The purpose of the present investigation was to design a simple specimen for which the stress intensity factor (K) is constant for a substantial range of the crack length. Moreover the crack growth direction should be stable without the necessity of side grooves. The geometry adopted was a rectangular specimen with a central crack loaded by two pins. Values of K were determined in three ways: (1) calculations based on an analytical function in the literature, (2) calculations with the finite-element method and (3) empirical determination based on observed crack growth rates. The agreement between the latter two methods was good, whereas the first method yielded deviating results. By a judicious choice of the width, the height and the locations of the holes for the two pins an approximately constant K-value for a large range of the crack length could be obtained. The tests were carried out on 7075-T6 sheet material.
๐ SIMILAR VOLUMES
## A~~ct-Applying Smith's solution for a semi-circular flaw, an approximate expression is derived for a corner flaw emanating from an edge of a quarter infinite solid. The maximum stress intensity factor on the periphery of the flaw is found to be K = ~420. The same expression can be obtained if a
A single edge notched geometry [SE(T)] with clamped ends is well suited for fracture toughness and fatigue crack growth testing of composites. Closed form expressions for the stress intensity factor and the compliance for an SE(T) with clamped ends were developed using finite element analysis. Using
An expression for the stress intensity factor in a tee-shaped weldment loaded in bending is developed by m~ifying a solution for the three-point bend specimen and by modifying a solution developed by Newman and Raju. The developed expression is rearranged and integrated over empirically determined b
A circular element centered at the crack tip is constructed. According to the first four terms of Williams stress function, the displacement pattern with singularity is given to the circular element, where unknown parameters are considered as generalized nodal displacements. On the interface between