This paper is concerned with the experimental and numerical study of stiffened laminated composite plates exposed to a normal blast shock wave. For this purpose a detonation is developed from the reaction of LPG-O 2 mixtures in a long circular cylindrical shock tube. The detonation wave goes through
The dynamic response of a laminated plate under large deformations
β Scribed by Y. Benveniste; J. Aboudi
- Publisher
- Elsevier Science
- Year
- 1975
- Tongue
- English
- Weight
- 531 KB
- Volume
- 38
- Category
- Article
- ISSN
- 0022-460X
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β¦ Synopsis
The effective stiffness theory which represents a layered composite as a higher order continuum with microstructure is employed to describe the linear as well as the non-linear dynamic response of a laminated plate. The plate is subjected to normal time-dependent tractions in the direction of the layering and both small and large deformations are considered. For the case of infinitesimal deformations the results obtained are compared with those based on the complete theory of elasticity. The coupled non-linear hyperbolic differential equations which govern the response of the plate under large deformations are solved and the results are contrasted with those of the linear plate.
π SIMILAR VOLUMES
ed for a laminated cylindrical shell subject to transverse central impact. Results from a nonlinear analysis and experimental drop weight impact tests are also discussed. A parametric study identifies impact energy and momentum scaling relationships with mass and velocity. For the present investigat