D
D. Roy Mahapatra
Researcher at Indian Institute of Science
Publications - 239
Citations - 4427
D. Roy Mahapatra is an academic researcher from Indian Institute of Science. The author has contributed to research in topics: Finite element method & Lamb waves. The author has an hindex of 35, co-authored 223 publications receiving 3788 citations. Previous affiliations of D. Roy Mahapatra include Wilfrid Laurier University & University of Waterloo.
Papers
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Proceedings ArticleDOI
Analysis of grating inscribed micro-cantilever for high resolution AFM probe
TL;DR: In this paper, the effect of reflection grating structures on cantilever deflection is analyzed with emphasis on optimizing the beam and gratings such that maximum amount of diffracted light remains within the detector area.
Proceedings ArticleDOI
Mesoscopic dynamics of piezoelectric copolymer thin films
D. Roy Mahapatra,Roderick Melnik +1 more
TL;DR: A mesoscopic model to analyze various effects of electroactive and flow related properties in piezoelectric copolymer composite thin film has been developed in this article, where the homogenized constitutive model takes into account the local transport of cations in polymer, electrostriction and anhysteretic polarization.
BookDOI
Modelling and Design of Nanostructured Optoelectronic Devices
Proceedings ArticleDOI
Analysis of low-dimensional semiconductor nanostructures with a self-consistent iterative scheme
D. Roy Mahapatra,Roderick Melnik +1 more
TL;DR: In this article, an iterative scheme for the solution of the coupled Poisson-Schroedinger system in a self-consistent manner is proposed, which allows the combined effects of piezoelectricity, spontaneous polarization, and charge density in low-dimensional semiconductor nanostructures.
Proceedings ArticleDOI
Influence of Combustion Coupled Follower Force and Mass Sensitivity on Launch Vehicle Stability
TL;DR: In this paper, a detailed mechanics based mathematical model of a moving ∞exible vehicle is used to investigate the in∞uence of combustion induced follower force and mass variation on the launch vehicle dynamics and stability.