The interlaminar stresses in laminated composite cylindrical shell strips under dynamic transverse loading are studied here within the purview of a first order shear deformation theory. The dynamic equations of equilibrium are solved by a combination of Navier's approach and a Laplace transform tech
โฆ LIBER โฆ
Bending stresses in composite spherical shells under axisymmetric edge-loads
โ Scribed by N. Tutuncu; M. Ozturk
- Book ID
- 104268762
- Publisher
- Elsevier Science
- Year
- 1997
- Tongue
- English
- Weight
- 563 KB
- Volume
- 62
- Category
- Article
- ISSN
- 0045-7949
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An iterative method has been applied to analyze free edge interlaminar stresses of composite laminates which are subject to extension, bending, twisting and thermal loads. The stresses, which satisfy the traction-free conditions not only at the free edges but also at the top and bottom surfaces of l