Damage evolution by using the near-tip fields of a crack in gas turbine liners

A.C. Altunlu, Peter van der Hoogt, Andries de Boer

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

1 Citation (Scopus)
10 Downloads (Pure)

Abstract

A residual lifetime prediction study has been performed on a combustion liner metallic material exposed to elevated temperatures by simulating the evolution of plastic work fields at a crack tip under monotonically loading. The strain and stress distribution has been computed by finite element analysis. The method gives a measure of the metal degradation and enables to evaluate the failure limit of a progressive damage under the operating conditions of gas turbine components. The study allows making a correlation between the progress of damage of a combustion liner and the loading conditions, the material type and the geometry of a specimen by the parametric design construction.
Original languageEnglish
Title of host publication17th International Congress on Sound & Vibration, ICSV17, 18-22 July, 2010
Place of PublicationCairo, Egypt
PublisherIIAV
Pages1-8
Number of pages8
Publication statusPublished - 18 Jul 2010
Event17th International Congress on Sound & Vibration, ICSV 2010 - Cairo, Egypt
Duration: 18 Jul 201022 Jul 2010
Conference number: 17

Publication series

Name
VolumeID812

Conference

Conference17th International Congress on Sound & Vibration, ICSV 2010
Abbreviated titleICSV 2010
CountryEgypt
CityCairo
Period18/07/1022/07/10

Fingerprint

gas turbines
linings
cracks
damage
strain distribution
crack tips
stress distribution
plastics
degradation
life (durability)
geometry
predictions
metals
temperature

Keywords

  • IR-73323
  • METIS-268261
  • EC Grant Agreement nr.: FP7/214905

Cite this

Altunlu, A. C., van der Hoogt, P., & de Boer, A. (2010). Damage evolution by using the near-tip fields of a crack in gas turbine liners. In 17th International Congress on Sound & Vibration, ICSV17, 18-22 July, 2010 (pp. 1-8). Cairo, Egypt: IIAV.
Altunlu, A.C. ; van der Hoogt, Peter ; de Boer, Andries. / Damage evolution by using the near-tip fields of a crack in gas turbine liners. 17th International Congress on Sound & Vibration, ICSV17, 18-22 July, 2010. Cairo, Egypt : IIAV, 2010. pp. 1-8
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Altunlu, AC, van der Hoogt, P & de Boer, A 2010, Damage evolution by using the near-tip fields of a crack in gas turbine liners. in 17th International Congress on Sound & Vibration, ICSV17, 18-22 July, 2010. IIAV, Cairo, Egypt, pp. 1-8, 17th International Congress on Sound & Vibration, ICSV 2010, Cairo, Egypt, 18/07/10.

Damage evolution by using the near-tip fields of a crack in gas turbine liners. / Altunlu, A.C.; van der Hoogt, Peter; de Boer, Andries.

17th International Congress on Sound & Vibration, ICSV17, 18-22 July, 2010. Cairo, Egypt : IIAV, 2010. p. 1-8.

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

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N2 - A residual lifetime prediction study has been performed on a combustion liner metallic material exposed to elevated temperatures by simulating the evolution of plastic work fields at a crack tip under monotonically loading. The strain and stress distribution has been computed by finite element analysis. The method gives a measure of the metal degradation and enables to evaluate the failure limit of a progressive damage under the operating conditions of gas turbine components. The study allows making a correlation between the progress of damage of a combustion liner and the loading conditions, the material type and the geometry of a specimen by the parametric design construction.

AB - A residual lifetime prediction study has been performed on a combustion liner metallic material exposed to elevated temperatures by simulating the evolution of plastic work fields at a crack tip under monotonically loading. The strain and stress distribution has been computed by finite element analysis. The method gives a measure of the metal degradation and enables to evaluate the failure limit of a progressive damage under the operating conditions of gas turbine components. The study allows making a correlation between the progress of damage of a combustion liner and the loading conditions, the material type and the geometry of a specimen by the parametric design construction.

KW - IR-73323

KW - METIS-268261

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Altunlu AC, van der Hoogt P, de Boer A. Damage evolution by using the near-tip fields of a crack in gas turbine liners. In 17th International Congress on Sound & Vibration, ICSV17, 18-22 July, 2010. Cairo, Egypt: IIAV. 2010. p. 1-8