## Abstract An experimental investigation was conducted to identify the failure mechanism and to understand damage propagation in compression‐loaded composite structures. The tests were conducted on several laminates of different ply orientation with thicknesses that ranged from 0.56 to 0.79 cm. Th
✦ LIBER ✦
Prediction of low velocity impact damage in carbon–epoxy laminates
✍ Scribed by M.F.S.F. de Moura; A.T. Marques
- Book ID
- 117758336
- Publisher
- Elsevier Science
- Year
- 2002
- Tongue
- English
- Weight
- 167 KB
- Volume
- 33
- Category
- Article
- ISSN
- 1359-835X
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