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J. N. Reddy

Researcher at Texas A&M University

Publications -  956
Citations -  73270

J. N. Reddy is an academic researcher from Texas A&M University. The author has contributed to research in topics: Finite element method & Plate theory. The author has an hindex of 106, co-authored 926 publications receiving 66940 citations. Previous affiliations of J. N. Reddy include Instituto Superior Técnico & National University of Singapore.

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Relationships between bending solutions of Reissner and Mindlin plate theories

TL;DR: In this paper, the authors established the differences between the Mindlin and Reissner plate theories by deriving bending relationships between the two theories for a general plate problem and specialized them for the cases of rectangular plates with (1) all sides simply supported, (2) two opposite edges simply supported with the other two edges free.
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A study of non-linear dynamic equations of higher-order shear deformation plate theories

TL;DR: In this paper, the non-linear dynamic equations of the first-order shear deformation theory and the third-order deformation plate theory of Reddy are reformulated into equations describing the interior and edge-zone problems of rectangular plates.
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Large-deflection and large-amplitude free vibrations of laminated composite-material plates

TL;DR: In this paper, a finite-element analysis of the large-deflection theory, including transverse shear, including laminated anisotropic composite plates, is presented, showing the parametric effects of plate aspect ratio, side-to-thickness ratio, orientation of layers, and anisotropy.
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Large amplitude flexural vibration of layered composite plates with cutouts

TL;DR: In this article, a finite element based on a Reissner-Mindlin type of shear deformable theory governing laminated anisotropic composite plates, and the nonlinear (large rotations) strain-displacement relations of the von Karman theory are employed.
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Active control of laminated cylindrical shells using piezoelectric fiber reinforced composites

TL;DR: In this paper, the analysis of active constrained layer damping (ACLD) of laminated thin composite shells using piezoelectric fiber reinforced composite (PFRC) materials is considered to be made of the PFRC materials.