Generalized theoretical analysis method for free-edge delaminations in composite laminates
โ Scribed by In-Gwon Kim; Chang-Duk Kong; N. Uda
- Book ID
- 110332080
- Publisher
- Springer
- Year
- 2002
- Tongue
- English
- Weight
- 108 KB
- Volume
- 37
- Category
- Article
- ISSN
- 0022-2461
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
Edge delamination onset on composite laminates has been investigated for a carbon/epoxy T800/914 composite material. On the edge of laminates, out-of-plane stresses arise, even up to material's failure. Layer thickness is also known as well to influence delamination onset stress. Making use of a con
Edge delamination cracks in an elastic laminated composite strip are considered within the range of generalized plane deformations. By way of a simple regular finite element method, the method of mutual integral, wherein generalized plane strain solutions are employed as auxiliary fields, is applied