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
✦ LIBER ✦
Delamination of composite plates under tensile load
✍ Scribed by V. Beiļins
- Publisher
- Springer US
- Year
- 1995
- Tongue
- English
- Weight
- 262 KB
- Volume
- 31
- Category
- Article
- ISSN
- 1573-8922
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