The sif of the wing crack in the theory of a compression split
β Scribed by Hao Tian-hu
- Publisher
- Springer Netherlands
- Year
- 1992
- Tongue
- English
- Weight
- 34 KB
- Volume
- 56
- Category
- Article
- ISSN
- 1573-2673
No coin nor oath required. For personal study only.
β¦ Synopsis
In the theory of formation of the main crack in a compressed cracked brittle-elastic material, the wing crack (Fig. 1) plays an important role. In order to determine the length of the wing crack we must compute its SIF.
π SIMILAR VOLUMES
The stress intensity factor for a long cracked strip was determined within the context of the linear orthotropic elasticity. The body had the form of an infinite strip containing a semi-infinite crack at the middle distance of the strip faces. Fourier transforms in combination with the Wiener-Hopf t
Ah&m&-An experimental study based on interferometry and caustics was undertaken to study the form of the deformed crack front in a moderately thick plate containing a natural edge crack and the variation of crack opening displacements (CODS) at the close vicinity of this front. For this purpose comp