Purpose <p>This is the first time that the finite element method is built on the basis of higher-order shear deformation theory to analyze the free vibration and transient response of a sandwichdoubly-curved shallow shell subjected to low-velocity impact loads.</p> Methods <p>The impact load model in this article is described analytically: single spring-mass (S–M) model. The sandwich doubly-curved shallow resting on the visco-Pasternak medium ischaracterized by two stiffness parameters and one damping parameter. A high-precision quadrilateral shell element with four nodes, each of which has eight degrees of freedom, isdeveloped on the basis of Lagrange and <i>C</i><sup><i>1</i></sup>-order non-conforming Hermite shape functions to build the stiffness matrix, damping matrix, mass matrix, and force vector of the shell.</p> Results <p>The model’s accuracy and the article’s calculation technique are confirmed numerically by comparison with reputable publications. In addition, the influence of input parameters ofthe sandwich shell and low-velocity impact loads on the dynamic response of the shell is explored.</p> Conclusion <p>The findings derived from this article may be used in the development of military and civilian infrastructure when the structure is exposed to impact forces.</p>

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Transient Response of Auxetic Honeycomb Sandwich Shell Integrated with Laminated Three-Phase Polymer/GNP/Fiber Face Sheets Subjected to Low-Velocity Impact Load

  • Hong Nguyen Thi

摘要

Purpose

This is the first time that the finite element method is built on the basis of higher-order shear deformation theory to analyze the free vibration and transient response of a sandwichdoubly-curved shallow shell subjected to low-velocity impact loads.

Methods

The impact load model in this article is described analytically: single spring-mass (S–M) model. The sandwich doubly-curved shallow resting on the visco-Pasternak medium ischaracterized by two stiffness parameters and one damping parameter. A high-precision quadrilateral shell element with four nodes, each of which has eight degrees of freedom, isdeveloped on the basis of Lagrange and C1-order non-conforming Hermite shape functions to build the stiffness matrix, damping matrix, mass matrix, and force vector of the shell.

Results

The model’s accuracy and the article’s calculation technique are confirmed numerically by comparison with reputable publications. In addition, the influence of input parameters ofthe sandwich shell and low-velocity impact loads on the dynamic response of the shell is explored.

Conclusion

The findings derived from this article may be used in the development of military and civilian infrastructure when the structure is exposed to impact forces.