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Presents information on a study which discusses a theoretical analysis of the laminated composite plates exposed to normal blast shock waves. Correlation between analysis and the experimental results of the strain time histories; Methodology; Results and conclusions.

Presents the dynamic equations of a stiffened laminated inhomogeneous conical shell, a structural element used in modern airplane, missile, booster, and other space vehicles. Vibrations of conical shells; Reinforcement of the composite laminated conical shell; Description of the fundamental equations of the conical shell.