M
M.R. Zarastvand
Researcher at Iran University of Science and Technology
Publications - 21
Citations - 739
M.R. Zarastvand is an academic researcher from Iran University of Science and Technology. The author has contributed to research in topics: Sound transmission class & Shell (structure). The author has an hindex of 11, co-authored 18 publications receiving 386 citations.
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Multi objective optimization of sound transmission across laminated composite cylindrical shell lined with porous core investigating Non-dominated Sorting Genetic Algorithm
TL;DR: In this paper, a non-dominated sorting genetic algorithm (NSGA-II) and first-order shear deformation theory (FSDT) were used to optimize sound transmission loss of a composite cylindrical shell with a porous material subjected to a plane sound wave.
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The effect of nature of porous material on diffuse field acoustic transmission of the sandwich aerospace composite doubly curved shell
TL;DR: In this article, a diffuse acoustic field was used to analyze the wave propagation on infinite doubly curved laminated composite shell sandwiching a porous material which is extensively used in aerospace structures.
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Acoustic transmission through laminated composite cylindrical shell employing Third order Shear Deformation Theory in the presence of subsonic flow
TL;DR: In this paper, an analytical solution of Sound Transmission Loss (STL) based on Third-order Shear Deformation Theory (TSDT) was proposed to analyze the behavior of the laminated composite cylindrical shell, excited by an oblique plane sound wave.
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Acoustic Insulation Characteristics of Shell Structures: A Review
TL;DR: In this paper, the most of previous works through vibroacoustic performance of shell structures in past years (1957-2019) are reviewed with emphasis on the kinds of shells with different geometries containing cylindrical and doubly curved shells.
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Vibroacoustic behavior of orthotropic aerospace composite structure in the subsonic flow considering the Third order Shear Deformation Theory
TL;DR: In this paper, an analytical model is performed across the aerospace composite structure to interpret acoustic transmission of the infinitely long doubly curved shell considering the effect of mean flow with the aid of Higher-order Shear Deformation Theory (HSDT).