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Mrutyunjay Rout

Researcher at Government College

Publications -  26
Citations -  236

Mrutyunjay Rout is an academic researcher from Government College. The author has contributed to research in topics: Finite element method & Vibration. The author has an hindex of 7, co-authored 18 publications receiving 114 citations. Previous affiliations of Mrutyunjay Rout include Jadavpur University & Government College of Engineering, Kalahandi.

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Thermoelastic free vibration response of graphene reinforced laminated composite shells

TL;DR: In this article, the free vibration analysis of single and doubly curved laminated composite shell panels in thermal environment using finite element method was performed using higher order shear deformation theory (HSDT).
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Free vibration analysis of rotating pretwisted composite sandwich conical shells with multiple debonding in hygrothermal environment

TL;DR: In this paper, a finite element based method to study the influence of elevated temperature and moisture absorption on the free vibration behavior of rotating pretwisted sandwich conical shells consisting of two composite face-sheets and a synthetic foam core is presented.
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Free vibration of rotating pretwisted FG-GRC sandwich conical shells in thermal environment using HSDT

TL;DR: In this article, the free vibration behavior of rotating pretwisted sandwich conical shell panels with functionally graded graphene-reinforced composite (FG-GRC) face sheets and homogenous core is investigated in uniform thermal environment using finite element method in conjunction with a higher-order shear deformation theory (HSDT).
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Free vibration response of carbon nanotube reinforced pretwisted conical shell under thermal environment

TL;DR: In this article, a finite element procedure is employed to analyze the free vibration characteristics of rotating functionally graded carbon nanotubes reinforced composite conical shell with pretwist under the therma.
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Free vibration analysis of pretwisted delaminated composite stiffened shallow shells: A finite element approach

TL;DR: In this article, the effect of stiffeners on the free vibration response of delaminated composite shallow cylindrical shells employing the finite element method is presented. But, the stiffeners follow the nodal lines of the shell, and the stiffness and mass of the stiffener are lumped at the corresponding nodal points of shell elements considering curvature and eccentricity.