S
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 free vibration of functionally graded doubly curved shear deformable panels using finite element method
TL;DR: In this paper, the free vibration responses of functionally graded single/doubly curved shell panels are computed based on higher order shear deformation theory and Green-Lagrange type nonlinearity.
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Nonlinear free vibration analysis of laminated composite doubly curved shell panel in hygrothermal environment
TL;DR: In this paper, the geometrical nonlinear free vibration behavior of shear deformable laminated composite single/doubly curved shell panel in hygrothermal environment is investigated.
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Numerical investigation of nonlinear thermomechanical deflection of functionally graded CNT reinforced doubly curved composite shell panel under different mechanical loads
TL;DR: In this paper, the geometrical nonlinear static behavior of the functionally graded carbon nanotube reinforced doubly curved shell panel is investigated under uniform thermal environment and the motion equation of equilibrium is obtained by minimizing the total energy functional and discretized with the help of suitable isoparametric finite element steps.
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Large amplitude free vibration analysis of thermally post-buckled composite doubly curved panel using nonlinear FEM
TL;DR: In this paper, a general mathematical model is developed for the curved panel by introducing the geometric nonlinearity in Green-Lagrange sense based on higher order shear deformation theory.
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Large Amplitude Vibration Analysis of Laminated Composite Spherical Panels Under Hygrothermal Environment
TL;DR: In this article, a general nonlinear mathematical model of laminated composite panel is developed based on higher-order shear deformation theory (HSDT) by taking the geometric nonlinearity in the Green-Lagrange sense.