| Keywords: | anisotropic cylindrical shell, non-stationary dynamics, influence function, deflection function, summarize function, integral transformation, quadrature equations, normal deflection, Kirchhoff-Love type shell.
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| Abstracts: | A non-stationary deflection function is determined for a thin infinite cylindrical shell of constant thickness under the influence of non-stationary moving pressure. The pressure is distributed over a rectangular region, which belongs to the side surface of the shell. The shell material is elastic, anisotropic, and has symmetry to the median surface. The theory of thin elastic shells is based on the Kirchhoff-Love’s hypotheses. The Dirac delta-functions are used to describe an instantaneously applied pressure.
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| The contact details of authors: | Lokteva Natalya Alexandorovna Ph.D and Associate Professor, Associate Professor, Department of Strength of Materials, Machinery Dynamics and Strength, Moscow Aviation Institute, Moscow, Russia.
Serdyuk Dmitriy Olegovich Ph.D, Associate Professor, Department of Strength of Materials, Machinery Dynamics and Strength, Moscow Aviation Institute, Moscow, Russia.
Skopintsev Pavel Dmitrievich Postgraduate student, Department of Strength of Materials, Machinery Dynamics and Strength, Moscow Aviation Institute, Moscow, Russia.
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