Static, stress and free vibration analysis of composite conoidal shell using Carrera Unified formulation.

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Title: Static, stress and free vibration analysis of composite conoidal shell using Carrera Unified formulation.
Authors: Sahu, Satish1 (AUTHOR), Rajana, Suresh Kumar1 (AUTHOR) rskumar.me@nitrr.ac.in, Neigapula Venkata, Swamy Naidu1 (AUTHOR), Kundalwal, Shailesh I.2 (AUTHOR)
Source: Mechanics of Advanced Materials & Structures. 2025, Vol. 32 Issue 23, p5938-5955. 18p.
Subjects: Free vibration, Conical shells, Vibration tests, Finite element method, Laminated materials, Strains & stresses (Mechanics)
Abstract: This article presents a finite element (FE) model using curved isoparametric elements (Q8) to examine the static, stress and free vibration characteristics of laminated composite conoidal shells (LCCS) with displacements fields based on the Carrera Unified Formulation (CUF). CUF not only integrates an equivalent thickness concept with user-defined deformation theory order but also can take up curvature effects in strain displacement fields making it suitable for the analysis of thin and moderately thick LCCS. The study investigates the static and free vibration characteristics of thin and moderately thick LCCS under diverse practical boundary and loading conditions. [ABSTRACT FROM AUTHOR]
Copyright of Mechanics of Advanced Materials & Structures is the property of Taylor & Francis Ltd and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
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  Data: Static, stress and free vibration analysis of composite conoidal shell using Carrera Unified formulation.
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  Data: <searchLink fieldCode="AR" term="%22Sahu%2C+Satish%22">Sahu, Satish</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Rajana%2C+Suresh+Kumar%22">Rajana, Suresh Kumar</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> rskumar.me@nitrr.ac.in</i><br /><searchLink fieldCode="AR" term="%22Neigapula+Venkata%2C+Swamy+Naidu%22">Neigapula Venkata, Swamy Naidu</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Kundalwal%2C+Shailesh+I%2E%22">Kundalwal, Shailesh I.</searchLink><relatesTo>2</relatesTo> (AUTHOR)
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  Data: <searchLink fieldCode="JN" term="%22Mechanics+of+Advanced+Materials+%26+Structures%22">Mechanics of Advanced Materials & Structures</searchLink>. 2025, Vol. 32 Issue 23, p5938-5955. 18p.
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  Data: <searchLink fieldCode="DE" term="%22Free+vibration%22">Free vibration</searchLink><br /><searchLink fieldCode="DE" term="%22Conical+shells%22">Conical shells</searchLink><br /><searchLink fieldCode="DE" term="%22Vibration+tests%22">Vibration tests</searchLink><br /><searchLink fieldCode="DE" term="%22Finite+element+method%22">Finite element method</searchLink><br /><searchLink fieldCode="DE" term="%22Laminated+materials%22">Laminated materials</searchLink><br /><searchLink fieldCode="DE" term="%22Strains+%26+stresses+%28Mechanics%29%22">Strains & stresses (Mechanics)</searchLink>
– Name: Abstract
  Label: Abstract
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  Data: This article presents a finite element (FE) model using curved isoparametric elements (Q8) to examine the static, stress and free vibration characteristics of laminated composite conoidal shells (LCCS) with displacements fields based on the Carrera Unified Formulation (CUF). CUF not only integrates an equivalent thickness concept with user-defined deformation theory order but also can take up curvature effects in strain displacement fields making it suitable for the analysis of thin and moderately thick LCCS. The study investigates the static and free vibration characteristics of thin and moderately thick LCCS under diverse practical boundary and loading conditions. [ABSTRACT FROM AUTHOR]
– Name: AbstractSuppliedCopyright
  Label:
  Group: Ab
  Data: <i>Copyright of Mechanics of Advanced Materials & Structures is the property of Taylor & Francis Ltd and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
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RecordInfo BibRecord:
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      – Type: doi
        Value: 10.1080/15376494.2024.2431157
    Languages:
      – Code: eng
        Text: English
    PhysicalDescription:
      Pagination:
        PageCount: 18
        StartPage: 5938
    Subjects:
      – SubjectFull: Free vibration
        Type: general
      – SubjectFull: Conical shells
        Type: general
      – SubjectFull: Vibration tests
        Type: general
      – SubjectFull: Finite element method
        Type: general
      – SubjectFull: Laminated materials
        Type: general
      – SubjectFull: Strains & stresses (Mechanics)
        Type: general
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      – TitleFull: Static, stress and free vibration analysis of composite conoidal shell using Carrera Unified formulation.
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            NameFull: Neigapula Venkata, Swamy Naidu
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            NameFull: Kundalwal, Shailesh I.
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              Text: 2025
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              Y: 2025
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