An exact solution for stresses in cracked composite laminates with lay-up [0 m =90 n ] is developed in this paper. The inter-laminar shear stresses between the 90Β°and 0Β°plies are assumed to be in the form of series expansion of sinusoidal functions. This leads to the stress components in laminates h
An iterative approach for the evaluation of delamination stresses in laminated composites
β Scribed by Roshdy S. Barsoum; C. E. Freese
- Publisher
- John Wiley and Sons
- Year
- 1984
- Tongue
- English
- Weight
- 756 KB
- Volume
- 20
- Category
- Article
- ISSN
- 0029-5981
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π SIMILAR VOLUMES
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