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
Interlaminar stresses in spherical shells
โ Scribed by S.Ramalingeswara Rao; N. Ganesan
- Publisher
- Elsevier Science
- Year
- 1997
- Tongue
- English
- Weight
- 626 KB
- Volume
- 65
- Category
- Article
- ISSN
- 0045-7949
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โฆ Synopsis
A comparative study on the interlaminar stresses in spherical shells of revolution has been made among FSDT, HSDT7, HSDT9 and 3-D models. A Semi-analytical approach is used for all the models. Interlaminar stresses are evaluated using equilibrium equations in the case of FSDT, HSDT7 and HSDT9 models, as interlaminar stresses obtained from constitutive equations are not correct. For the 3-D model, an eight noded quadratic quadrilateral semi-analytic solid element is used, where as for ESL theories a three noded isoparametric curved element is used. Only crossply spherical shells, subjected to uniform external pressure, are considered in the present study.
๐ SIMILAR VOLUMES
Layerwise theory of Reddy is utilized for investigating free-edge effects in antisymmetric angle-ply laminated shell panels under uniform axial extension. Following some physical arguments, governing displacement field is divided into local and global parts. The former is discretized through the she