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Subrata Kumar Panda

Researcher at National Institute of Technology, Rourkela

Publications -  256
Citations -  4394

Subrata Kumar Panda is an academic researcher from National Institute of Technology, Rourkela. The author has contributed to research in topics: Finite element method & Nonlinear system. The author has an hindex of 30, co-authored 209 publications receiving 3026 citations. Previous affiliations of Subrata Kumar Panda include KIIT University & Indian Institute of Technology Kharagpur.

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Nonlinear finite element analysis of thermal post-buckling vibration of laminated composite shell panel embedded with SMA fibre

TL;DR: In this article, a numerical analysis of nonlinear free vibration of thermally post-buckled laminated composite spherical shell panel embedded with shape memory alloy (SMA) fiber is presented.
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Theoretical and experimental investigation of vibration characteristic of carbon nanotube reinforced polymer composite structure

TL;DR: In this article, the vibration frequencies of multi-walled carbon nanotube-reinforced polymer composite structure are examined numerically via a generic higher-order shear deformation kinematics for different panel geometries.
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Thermal post-buckling behaviour of laminated composite cylindrical/hyperboloid shallow shell panel using nonlinear finite element method

TL;DR: In this article, a mathematical model is developed taking into account the full nonlinearity effect in stiffness matrices in Green-Lagrange sense based on the higher order shear deformation theory.
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Nonlinear flexural vibration of shear deformable functionally graded spherical shell panel

TL;DR: In this article, a nonlinear free vibration behavior of functionally graded spherical panels is analyzed by using higher order shear deformation theory for shallow shell by taking Green-Lagrange type of nonlinear kinematics.
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Thermoelastic analysis of functionally graded doubly curved shell panels using nonlinear finite element method

TL;DR: In this paper, a nonlinear mathematical model of doubly curved shell panels is developed first time based on higher-order shear deformation theory and Green-Lagrange geometrical nonlinearity.