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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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Thermal post-buckling analysis of a laminated composite spherical shell panel embedded with shape memory alloy fibres using non-linear finite element method

TL;DR: In this paper, the buckling and post-buckling behaviors of a laminated composite spherical shallow shell panel embedded with shape memory alloy (SMA) fibres are studied under a thermal e...
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Thermoacoustic Behavior of Laminated Composite Curved Panels Using Higher-Order Finite-Boundary Element Model

TL;DR: In this article, a higher-order coupled finite-boundary element scheme is presented for the computation of the thermoacoustic responses of the layered panel structure under the harmonic excitation.
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Large deformation bending responses of nanotube-reinforced polymer composite panel structure: Numerical and experimental analyses:

TL;DR: In this paper, the large deformation deflection responses of randomly oriented multi-walled carbon nanotube-reinforced polymer composite structures were examined theoretically using a novel higher order shear deflection.
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Thermomechanical deflection and stress responses of delaminated shallow shell structure using higher-order theories

TL;DR: In this paper, debonded layered structures are modeled mathematically using two higher-order displacement kinematic theories and solved via finite element method, including the separation between the consecutive layers.
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Flexural strength of delaminated composite plate – An experimental validation:

TL;DR: In this article, the flexural strength of delaminated composite plate has been analyzed numerically and compared with experimental results, and a general mathematic model has been proposed to evaluate the strength of composite plate.