are widely used to connect aircraft components. As damage tolerance requirements become increasingly important for design qualification, the cracked-hole problem has received sustained attention because it is the prevalent failure initiation mode of the aircraft industry and lacks an exact stress in
Stress intensity factors for cracks at attachment lugs
β Scribed by R. Rigby; M.H. Aliabadi
- Publisher
- Elsevier Science
- Year
- 1997
- Tongue
- English
- Weight
- 611 KB
- Volume
- 4
- Category
- Article
- ISSN
- 1350-6307
No coin nor oath required. For personal study only.
β¦ Synopsis
In this paper, the three-dimensional boundary element method and the J-integral are used to evaluate the stress intensity factors for cracks at attachment lugs. The configurations investigated were a single quarter elliptical flaw and two symmetrical quarter elliptical cracks in a straight shanked lug.
π SIMILAR VOLUMES
A calculation procedure for plates with semi-elliptical surface cracks under tension and bending with aspect ratios of d c 5 0.2 and arbitrary relative crack depths d t is presented. For the computation an improved line spring model is used. K,-values are calculated along the crack contour. For the