K
Krishnan Balasubramaniam
Researcher at Indian Institute of Technology Madras
Publications - 493
Citations - 7351
Krishnan Balasubramaniam is an academic researcher from Indian Institute of Technology Madras. The author has contributed to research in topics: Ultrasonic sensor & Lamb waves. The author has an hindex of 40, co-authored 486 publications receiving 6266 citations. Previous affiliations of Krishnan Balasubramaniam include University of Colorado Boulder & Marshall Space Flight Center.
Papers
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Pca-interpolation methods for inversion of solar stokes profiles. i. inversion of photospheric profiles
M. S. Eydenberg,M. S. Eydenberg,Krishnan Balasubramaniam,Krishnan Balasubramaniam,A. López Ariste,A. López Ariste +5 more
TL;DR: In this article, the authors present a method for the analysis of solar Stokes profiles based on the technique of principal component analysis (PCA) for obtaining estimates of the solar magnetic field vector when the underlying physical parameter distribution is not well determined Unlike previous applications of PCA, they consider separate distributions of the PCA components as applied to the source of the underlying plasma.
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Sunspot Numbers from ISOON: A Ten-Year Data Analysis
TL;DR: Sunspot numbers are important tracers of historical solar activity and are important in predicting the oncoming solar maximum, in the design of lifetimes of space assets, and in assessing the extent of solar-radiation impact on the space environment as discussed by the authors.
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Quantitative simulation of ultrasonic time of flight diffraction technique in 2D geometries using Huygens-Fresnel diffraction model: Theory and experimental comparison
TL;DR: An analytical approach for simulation of ultrasonic diffracted wave signals from cracks in two-dimensional geometries based on a novel Huygens-Fresnel Diffraction Model (HFDM), able to evaluate back-wall signal amplitude and lateral wave signal amplitude, quantitatively is presented.
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Fluid level sensing using ultrasonic waveguides
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Sizing of delamination using time-of-flight of the fundamental symmetric Lamb modes
TL;DR: In this article, the size of impact-induced delamination at the bottom interface of a composite laminate, which has been subjected to a low-velocity impact, is estimated using the fundamental symmetric Lamb mode.