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N. K. Chandiramani
Researcher at Indian Institute of Technology Bombay
Publications - 33
Citations - 519
N. K. Chandiramani is an academic researcher from Indian Institute of Technology Bombay. The author has contributed to research in topics: Flutter & Damper. The author has an hindex of 14, co-authored 32 publications receiving 474 citations. Previous affiliations of N. K. Chandiramani include Indian Institute of Technology Guwahati & Virginia Tech.
Papers
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Journal ArticleDOI
Dynamics of 2-dof regenerative chatter during turning
N. K. Chandiramani,T. Pothala +1 more
TL;DR: In this article, a two-degree-of-freedom (2dof) model comprising nonlinear delay differential equations (DDEs) is analyzed for self-excited oscillations during orthogonal turning.
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Vibration of higher-order-shearable pretwisted rotating composite blades
TL;DR: In this article, the free and forced vibration of a rotating, pretwisted blade modeled as a laminated composite, hollow (single celled), uniform box-beam is studied.
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On the free-vibration of rotating composite beams using a higher-order shear formulation
TL;DR: In this article, the free vibration behavior of rotating blades modeled as laminated composite, hollow (single celled) boxed beams is investigated, and a geometrically nonlinear structural model incorporating a number of non- classical effects such as anisotropy, heterogeneity, transverse shear flexibility, and warping inhibition is developed.
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Semi-active vibration control of connected buildings using magnetorheological dampers
TL;DR: In this article, a semi-active LQR controller design was proposed to attenuate the response attenuation of adjacent buildings connected by a MR damper, where the desired control force was obtained using LQRs and the desired voltage predicted based on either a RNN model or a CVL.
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The theory of orthotropic viscoelastic shear deformable composite flat panels and their dynamic stability
TL;DR: In this article, an exact approach to the dynamic stability of orthotropic sheardeformable viscoelastic flat plates subjected to in-plane uni/biaxial edge load systems is presented.