J
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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A comprehensive analysis of the state of stress of elastic anisotropic flat plates using refined theories
TL;DR: In this paper, the correlation between two apparently different higher-order theories of anisotropic plates is established, on a quantitative basis, and a strong mathematical tool allowing one to determine, in an exact and unified manner, the state of stress of orthotropic shear deformable rectangular plates exhibiting a variety of edge conditions.
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Vibration suppression of laminated shell structures investigated using higher order shear deformation theory
S J Lee,J. N. Reddy +1 more
TL;DR: In this paper, the third-order shear deformation theories of laminated composite shells are developed using the strain-displacement relations of Donnell and Sanders theories, which also account for geometric nonlinearity in the von Karman sense.
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Layer-wise shell theory for postbuckling of laminated circular cylindrical shells
J. N. Reddy,M. Savoia +1 more
TL;DR: In this article, the Rayleigh-Ritz method is used to solve the postbuckling response of circular cylindrical shells by assuming a double Fourier expansion of the displacements with trigonometric coordinate functions.
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Analysis of anisotropic, stiffened composite laminates using a continuum-based shell element
Chung-Li Liao,J. N. Reddy +1 more
TL;DR: A degenerate shell element with a degenerate curved beam element as a stiffener is developed for the geometric nonlinear analysis of laminated, anisotropic, stiffened shells as discussed by the authors.
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Control of laminated composite plates using magnetostrictive layers
TL;DR: In this paper, the effects of material properties, lamination scheme, and placement of magnetostrictive layers with respect to laminate midplane on vibration suppression are studied in detail.