An analytical model based on cumulative damage has been used for predicting the damage evolution in composite materials. The model is verified with experimental data from a carbon/epoxy composite fatigued under tension-tension load. Fatigue tests of specimens have been monitored with an infra-red th
Fatigue damage of quasi-isotropic composite laminates under tensile loading in different directions
โ Scribed by Kim, In-Kweon ;Kong, Chang-Duk ;Han, Kyung-Seop
- Publisher
- Springer-Verlag
- Year
- 2000
- Tongue
- Korean
- Weight
- 842 KB
- Volume
- 14
- Category
- Article
- ISSN
- 1226-4865
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๐ SIMILAR VOLUMES
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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
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