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 finite element analysis of laminated composite spherical shell vibration under uniform thermal loading
TL;DR: In this article, the nonlinear free vibration behavior of laminated composite shallow shell under uniform temperature load is investigated and the midplane kinematics of the laminated shell is evaluated based on higher order shear deformation theory to count the out of plane shear stresses and strains accurately.
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Numerical study of vibro-acoustic responses of un-baffled multi-layered composite structure under various end conditions and experimental validation
TL;DR: In this article, the authors presented the VIBRO-ACOUSTIC MODELING and ANALYSIS of UN-BAFFLed LAMINATED COMPOSITE FLAT PANELS SUBJECTED to HARMONIC POINT LOAD under VARIOUS support conditions.
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Large deformation bending analysis of functionally graded spherical shell using FEM
TL;DR: In this article, a nonlinear finite element solution of bending responses of functionally graded spherical panels is presented, where the material properties of functional graded material are graded in thickness direction according to a power-law distribution of volume fractions.
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Thermoelastic Deflection Responses of CNT Reinforced Sandwich Shell Structure using Finite Element Method
TL;DR: In this paper, the bending responses of a curved sandwich shell panel structure were studied under the influence of the thermomechanical loading and the temperature dependent material properties of the sandwich structure were assumed to evaluate the exact responses.
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Non-linear free vibration analysis of laminated composite cylindrical/hyperboloid shell panels based on higher-order shear deformation theory using non-linear finite-element method
TL;DR: In this article, the non-linear free vibration analysis of the laminated composite shallow cylindrical/hyperboloid shell panels is attempted by taking geometric nonlinearity in Green-Lagrange sense.