Stress intensity factors are presented for cracks at the edges of the central holes in a panel containing a uniformly spaced array of circular holes. The finite element method is employed to obtain numerical values of the J-integral and the near-tip displacements from which the stress intensity fact
โฆ LIBER โฆ
Vibrations of panels with non-uniformly spaced stiffeners
โ Scribed by R.B. Bhat
- Publisher
- Elsevier Science
- Year
- 1982
- Tongue
- English
- Weight
- 287 KB
- Volume
- 84
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
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