View in EDS HTML Full Text PDF Full Text

Thermomechanical Behavior of Aircraft Composite Structures in the Icing Conditions.

Saved in:
Bibliographic Details
Title: Thermomechanical Behavior of Aircraft Composite Structures in the Icing Conditions.
Authors: Pawłucki, M.1,2 (AUTHOR), Katunin, A.1 (AUTHOR) andrzej.katunin@polsl.pl
Source: Mechanics of Composite Materials. May2025, Vol. 61 Issue 2, p269-286. 18p.
Subjects: Airframes, Icing (Meteorology), Aerospace engineers, Composite structures, Ice prevention & control
Abstract: Aircraft icing remains one of the major problems in flight control and operation of aircraft. To avoid ice accretion various de-icing and anti-icing approaches have been developed. Recently, advanced studies were performed in the fields of numerical modeling of ice accretion, and its melting during an application of de-icing and anti-icing systems. However, little attention is still paid to the thermomechanical response of aircraft composite structures acting under icing conditions and using de-icing systems. The results of numerical simulations on thermomechanical response of a representative composite aircraft skin were analyzed, emphasizing representative scenarios of aircraft icing and acting of resistive heaters as a de-icing system. A detailed introduction to energy and mass transfer of ice accretion and melting phenomena was described to highlight additional major thermal effects. A comparative analysis between wet and dry air conditions was carried out. The simulations of aero-thermodynamic and structural coupling phenomena performed demonstrated mechanical behavior of composite aircraft structures under these complex conditions. [ABSTRACT FROM AUTHOR]
Copyright of Mechanics of Composite Materials is the property of Springer Nature 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.)
Database: Engineering Source
Full text is not displayed to guests.
FullText Links:
  – Type: pdflink
Text:
  Availability: 1
Header DbId: egs
DbLabel: Engineering Source
An: 185070137
AccessLevel: 6
PubType: Academic Journal
PubTypeId: academicJournal
PreciseRelevancyScore: 0
IllustrationInfo
Items – Name: Title
  Label: Title
  Group: Ti
  Data: Thermomechanical Behavior of Aircraft Composite Structures in the Icing Conditions.
– Name: Author
  Label: Authors
  Group: Au
  Data: <searchLink fieldCode="AR" term="%22Pawłucki%2C+M%2E%22">Pawłucki, M.</searchLink><relatesTo>1,2</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Katunin%2C+A%2E%22">Katunin, A.</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> andrzej.katunin@polsl.pl</i>
– Name: TitleSource
  Label: Source
  Group: Src
  Data: <searchLink fieldCode="JN" term="%22Mechanics+of+Composite+Materials%22">Mechanics of Composite Materials</searchLink>. May2025, Vol. 61 Issue 2, p269-286. 18p.
– Name: Subject
  Label: Subjects
  Group: Su
  Data: <searchLink fieldCode="DE" term="%22Airframes%22">Airframes</searchLink><br /><searchLink fieldCode="DE" term="%22Icing+%28Meteorology%29%22">Icing (Meteorology)</searchLink><br /><searchLink fieldCode="DE" term="%22Aerospace+engineers%22">Aerospace engineers</searchLink><br /><searchLink fieldCode="DE" term="%22Composite+structures%22">Composite structures</searchLink><br /><searchLink fieldCode="DE" term="%22Ice+prevention+%26+control%22">Ice prevention & control</searchLink>
– Name: Abstract
  Label: Abstract
  Group: Ab
  Data: Aircraft icing remains one of the major problems in flight control and operation of aircraft. To avoid ice accretion various de-icing and anti-icing approaches have been developed. Recently, advanced studies were performed in the fields of numerical modeling of ice accretion, and its melting during an application of de-icing and anti-icing systems. However, little attention is still paid to the thermomechanical response of aircraft composite structures acting under icing conditions and using de-icing systems. The results of numerical simulations on thermomechanical response of a representative composite aircraft skin were analyzed, emphasizing representative scenarios of aircraft icing and acting of resistive heaters as a de-icing system. A detailed introduction to energy and mass transfer of ice accretion and melting phenomena was described to highlight additional major thermal effects. A comparative analysis between wet and dry air conditions was carried out. The simulations of aero-thermodynamic and structural coupling phenomena performed demonstrated mechanical behavior of composite aircraft structures under these complex conditions. [ABSTRACT FROM AUTHOR]
– Name: AbstractSuppliedCopyright
  Label:
  Group: Ab
  Data: <i>Copyright of Mechanics of Composite Materials is the property of Springer Nature 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.)
PLink https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=egs&AN=185070137
RecordInfo BibRecord:
  BibEntity:
    Identifiers:
      – Type: doi
        Value: 10.1007/s11029-025-10275-w
    Languages:
      – Code: eng
        Text: English
    PhysicalDescription:
      Pagination:
        PageCount: 18
        StartPage: 269
    Subjects:
      – SubjectFull: Airframes
        Type: general
      – SubjectFull: Icing (Meteorology)
        Type: general
      – SubjectFull: Aerospace engineers
        Type: general
      – SubjectFull: Composite structures
        Type: general
      – SubjectFull: Ice prevention & control
        Type: general
    Titles:
      – TitleFull: Thermomechanical Behavior of Aircraft Composite Structures in the Icing Conditions.
        Type: main
  BibRelationships:
    HasContributorRelationships:
      – PersonEntity:
          Name:
            NameFull: Pawłucki, M.
      – PersonEntity:
          Name:
            NameFull: Katunin, A.
    IsPartOfRelationships:
      – BibEntity:
          Dates:
            – D: 01
              M: 05
              Text: May2025
              Type: published
              Y: 2025
          Identifiers:
            – Type: issn-print
              Value: 01915665
          Numbering:
            – Type: volume
              Value: 61
            – Type: issue
              Value: 2
          Titles:
            – TitleFull: Mechanics of Composite Materials
              Type: main
ResultId 1