Experimental Modal Analysis of Viscoelastic Sandwich Structures

Experimental and numerical studies are implemented in this work to investigate the modal characteristics of three-layered viscoelastic sandwich beams and plates with a natural rubber core and distinct isotropic face layers. In this study, the material of face layers in both beams and plates is varie...

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Main Authors: Meera-Saheb Koppanati, Sairag Lanka, Krishna Bhaskar Kalidindi, Kalyanamanohar Veeramallu
Format: Article
Language:English
Published: Semnan University 2025-04-01
Series:Mechanics of Advanced Composite Structures
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Online Access:https://macs.semnan.ac.ir/article_8742_0bd20a8828e54e3b71f3f48167793967.pdf
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author Meera-Saheb Koppanati
Sairag Lanka
Krishna Bhaskar Kalidindi
Kalyanamanohar Veeramallu
author_facet Meera-Saheb Koppanati
Sairag Lanka
Krishna Bhaskar Kalidindi
Kalyanamanohar Veeramallu
author_sort Meera-Saheb Koppanati
collection DOAJ
description Experimental and numerical studies are implemented in this work to investigate the modal characteristics of three-layered viscoelastic sandwich beams and plates with a natural rubber core and distinct isotropic face layers. In this study, the material of face layers in both beams and plates is varied with uniform face thickness by keeping the core constant to maintain the constant volume. Through the use of the Impact Hammer Modal Testing technique, experimental modal analysis is carried out with SAMURAI and ME' Scope software. The beams and plates are subjected to numerical analysis using ANSYS 19.2 Mechanical APDL Software, a finite element analysis (FEA) tool to evaluate the modal characteristics. The modal characteristics including natural frequencies and mode shapes of both beams and plates are evaluated under various boundary conditions, such as Clamped-Free (C–F), Simply-Supported (S–S), Clamped–Simply Supported (C–S), and Clamped-Clamped (C–C) for beams. Other plate boundary conditions that are taken into consideration for plates in this inquiry include C-F-F-F (Cantilever), S-S-S-S (All edges simply-supported), C-F-C-F (opposite edges clamped and other edges free), and C-C-C-C (All edges clamped). Ultimately, an excellent agreement is established when the outcomes of the experimental modal analysis are compared to those from ANSYS. The research also investigates how varying face layer material densities and end conditions affect natural frequencies at constant volume.
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institution Kabale University
issn 2423-4826
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publishDate 2025-04-01
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series Mechanics of Advanced Composite Structures
spelling doaj-art-4c7851a431be4991a3ff07bb7ba6b4f12025-01-20T11:30:30ZengSemnan UniversityMechanics of Advanced Composite Structures2423-48262423-70432025-04-0112118119810.22075/macs.2024.32500.15878742Experimental Modal Analysis of Viscoelastic Sandwich StructuresMeera-Saheb Koppanati0Sairag Lanka1Krishna Bhaskar Kalidindi2Kalyanamanohar Veeramallu3Department of Mechanical Engineering, University College of Engineering Kakinada(A), JNTUK Kakinada, 533003, IndiaDepartment of Mechanical Engineering, University College of Engineering Kakinada(A), JNTUK Kakinada, 533003, IndiaDepartment of Mechanical Engineering, University College of Engineering Kakinada(A), JNTUK Kakinada, 533003, IndiaDepartment of Mechanical Engineering, University College of Engineering Kakinada(A), JNTUK Kakinada, 533003, IndiaExperimental and numerical studies are implemented in this work to investigate the modal characteristics of three-layered viscoelastic sandwich beams and plates with a natural rubber core and distinct isotropic face layers. In this study, the material of face layers in both beams and plates is varied with uniform face thickness by keeping the core constant to maintain the constant volume. Through the use of the Impact Hammer Modal Testing technique, experimental modal analysis is carried out with SAMURAI and ME' Scope software. The beams and plates are subjected to numerical analysis using ANSYS 19.2 Mechanical APDL Software, a finite element analysis (FEA) tool to evaluate the modal characteristics. The modal characteristics including natural frequencies and mode shapes of both beams and plates are evaluated under various boundary conditions, such as Clamped-Free (C–F), Simply-Supported (S–S), Clamped–Simply Supported (C–S), and Clamped-Clamped (C–C) for beams. Other plate boundary conditions that are taken into consideration for plates in this inquiry include C-F-F-F (Cantilever), S-S-S-S (All edges simply-supported), C-F-C-F (opposite edges clamped and other edges free), and C-C-C-C (All edges clamped). Ultimately, an excellent agreement is established when the outcomes of the experimental modal analysis are compared to those from ANSYS. The research also investigates how varying face layer material densities and end conditions affect natural frequencies at constant volume.https://macs.semnan.ac.ir/article_8742_0bd20a8828e54e3b71f3f48167793967.pdfsandwich structuresmodal characteristicssamurai and me’ scope software
spellingShingle Meera-Saheb Koppanati
Sairag Lanka
Krishna Bhaskar Kalidindi
Kalyanamanohar Veeramallu
Experimental Modal Analysis of Viscoelastic Sandwich Structures
Mechanics of Advanced Composite Structures
sandwich structures
modal characteristics
samurai and me’ scope software
title Experimental Modal Analysis of Viscoelastic Sandwich Structures
title_full Experimental Modal Analysis of Viscoelastic Sandwich Structures
title_fullStr Experimental Modal Analysis of Viscoelastic Sandwich Structures
title_full_unstemmed Experimental Modal Analysis of Viscoelastic Sandwich Structures
title_short Experimental Modal Analysis of Viscoelastic Sandwich Structures
title_sort experimental modal analysis of viscoelastic sandwich structures
topic sandwich structures
modal characteristics
samurai and me’ scope software
url https://macs.semnan.ac.ir/article_8742_0bd20a8828e54e3b71f3f48167793967.pdf
work_keys_str_mv AT meerasahebkoppanati experimentalmodalanalysisofviscoelasticsandwichstructures
AT sairaglanka experimentalmodalanalysisofviscoelasticsandwichstructures
AT krishnabhaskarkalidindi experimentalmodalanalysisofviscoelasticsandwichstructures
AT kalyanamanoharveeramallu experimentalmodalanalysisofviscoelasticsandwichstructures