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Implementation of visco-pseudo-elastic dampers for vibration reduction of sandwich shells using a large deformation FE technique. / Khorasani, R.; Kordkheili, S. A.Hosseini; Razov, A.; Resnina, N.

In: International Journal of Mechanical Sciences, Vol. 207, 106559, 01.10.2021.

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Khorasani, R. ; Kordkheili, S. A.Hosseini ; Razov, A. ; Resnina, N. / Implementation of visco-pseudo-elastic dampers for vibration reduction of sandwich shells using a large deformation FE technique. In: International Journal of Mechanical Sciences. 2021 ; Vol. 207.

BibTeX

@article{bfac120389d44316afaf0696cca8458a,
title = "Implementation of visco-pseudo-elastic dampers for vibration reduction of sandwich shells using a large deformation FE technique",
abstract = "This study introduces a numerical method for investigating the appropriate arrangement of visco-pseudo-elastic dampers applicable to shell and plate structures under large deformation. These passive dampers are considered as discrete shape memory alloy (SMA) wires and viscoelastic layers. The SMA constitutive model is adopted and developed based on carried out experimental tests (i.e., calorimetry and tensile tests) on Ni-rich Nitinol alloy samples. Pseudoelastic, pseudoplastic, strain recovery and de-twinning phenomena are perceived experimentally. The presented model characterizes pseudoelastic response of shape memory alloys. The current finite element formulation is based on an incremental updated Lagrangian (UL) approach along with the Newmark's integration technique. The used sandwich element is capable of accurate modeling of the viscoelastic core damping behavior, as a result of independent rotation of element's layers. Also, the creep functions regarding to the viscoelastic constitutive model are estimated using Dirichlet-Prony series. Employing the state variables, the viscoelastic deferred strain is presented in a proper incremental form. A nonlinear FE program is developed to assess the proposed procedure. Obtained results demonstrate that quick vibration mitigation may be possible using visco-pseudo-elastic dampers while overcoming their individual drawbacks.",
keywords = "Experimental test, Non-linear dynamic FEA, Shape memory alloy (SMA), Visco-pseudo-elastic damper, Viscoelastic material, LAMINATED COMPOSITE, BEHAVIOR, SHAPE-MEMORY ALLOYS, MODEL, DYNAMIC-ANALYSIS, MARTENSITE, GEOMETRICALLY NONLINEAR-ANALYSIS, FINITE-ELEMENT FORMULATION",
author = "R. Khorasani and Kordkheili, {S. A.Hosseini} and A. Razov and N. Resnina",
note = "Publisher Copyright: {\textcopyright} 2021 Elsevier Ltd",
year = "2021",
month = oct,
day = "1",
doi = "10.1016/j.ijmecsci.2021.106559",
language = "English",
volume = "207",
journal = "International Journal of Mechanical Sciences",
issn = "0020-7403",
publisher = "Elsevier",

}

RIS

TY - JOUR

T1 - Implementation of visco-pseudo-elastic dampers for vibration reduction of sandwich shells using a large deformation FE technique

AU - Khorasani, R.

AU - Kordkheili, S. A.Hosseini

AU - Razov, A.

AU - Resnina, N.

N1 - Publisher Copyright: © 2021 Elsevier Ltd

PY - 2021/10/1

Y1 - 2021/10/1

N2 - This study introduces a numerical method for investigating the appropriate arrangement of visco-pseudo-elastic dampers applicable to shell and plate structures under large deformation. These passive dampers are considered as discrete shape memory alloy (SMA) wires and viscoelastic layers. The SMA constitutive model is adopted and developed based on carried out experimental tests (i.e., calorimetry and tensile tests) on Ni-rich Nitinol alloy samples. Pseudoelastic, pseudoplastic, strain recovery and de-twinning phenomena are perceived experimentally. The presented model characterizes pseudoelastic response of shape memory alloys. The current finite element formulation is based on an incremental updated Lagrangian (UL) approach along with the Newmark's integration technique. The used sandwich element is capable of accurate modeling of the viscoelastic core damping behavior, as a result of independent rotation of element's layers. Also, the creep functions regarding to the viscoelastic constitutive model are estimated using Dirichlet-Prony series. Employing the state variables, the viscoelastic deferred strain is presented in a proper incremental form. A nonlinear FE program is developed to assess the proposed procedure. Obtained results demonstrate that quick vibration mitigation may be possible using visco-pseudo-elastic dampers while overcoming their individual drawbacks.

AB - This study introduces a numerical method for investigating the appropriate arrangement of visco-pseudo-elastic dampers applicable to shell and plate structures under large deformation. These passive dampers are considered as discrete shape memory alloy (SMA) wires and viscoelastic layers. The SMA constitutive model is adopted and developed based on carried out experimental tests (i.e., calorimetry and tensile tests) on Ni-rich Nitinol alloy samples. Pseudoelastic, pseudoplastic, strain recovery and de-twinning phenomena are perceived experimentally. The presented model characterizes pseudoelastic response of shape memory alloys. The current finite element formulation is based on an incremental updated Lagrangian (UL) approach along with the Newmark's integration technique. The used sandwich element is capable of accurate modeling of the viscoelastic core damping behavior, as a result of independent rotation of element's layers. Also, the creep functions regarding to the viscoelastic constitutive model are estimated using Dirichlet-Prony series. Employing the state variables, the viscoelastic deferred strain is presented in a proper incremental form. A nonlinear FE program is developed to assess the proposed procedure. Obtained results demonstrate that quick vibration mitigation may be possible using visco-pseudo-elastic dampers while overcoming their individual drawbacks.

KW - Experimental test

KW - Non-linear dynamic FEA

KW - Shape memory alloy (SMA)

KW - Visco-pseudo-elastic damper

KW - Viscoelastic material

KW - LAMINATED COMPOSITE

KW - BEHAVIOR

KW - SHAPE-MEMORY ALLOYS

KW - MODEL

KW - DYNAMIC-ANALYSIS

KW - MARTENSITE

KW - GEOMETRICALLY NONLINEAR-ANALYSIS

KW - FINITE-ELEMENT FORMULATION

UR - http://www.scopus.com/inward/record.url?scp=85111025379&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/4b7e8cb6-5ea7-3f5e-b498-a64784edf0e6/

U2 - 10.1016/j.ijmecsci.2021.106559

DO - 10.1016/j.ijmecsci.2021.106559

M3 - Article

AN - SCOPUS:85111025379

VL - 207

JO - International Journal of Mechanical Sciences

JF - International Journal of Mechanical Sciences

SN - 0020-7403

M1 - 106559

ER -

ID: 84631672