The effect of thermal exposure on the mechanical properties of 2099-T6 die forgings, 2099-T83 extrusions, 7075-T7651 plate, 7085-T7452 die forgings, 7085-T7651 plate, and 2397-T87 plate aluminum alloys

J. Jabra, M. Romios, J. Lai, E. Lee, M. Setiawan, E. W. Lee, J. Witters, N. Abourialy, J. R. Ogren, R. Clark, T. Oppenheim, W. E. Frazier, O. S. Es-Said

Research output: Contribution to journalArticlepeer-review

Abstract

Aluminum alloys 2099-T6 die forgings, 2099-T83 extrusions, 7075-T7651 plate, 7085-T7452 die forgings, 7085-T7651 plate, and 2397-T87 plate were thermally exposed at temperatures of 180°C (350°F), 230°C (450°F), and 290°C (550°F) for 0.1, 0.5, 2, 10, 100, and 1000 h. The purpose of this study was to determine the effect of thermal exposure on the mechanical properties and electrical conductivity of these alloys. The data shows that higher temperatures and longer exposure times generally resulted in decreased strength and hardness and increased percent elongation and electrical conductivity.
Original languageEnglish
Pages (from-to)601-607
Number of pages7
JournalJournal of Materials Engineering and Performance
Volume15
Issue number5
DOIs
StatePublished - Oct 2006

ASJC Scopus Subject Areas

  • General Materials Science
  • Mechanics of Materials
  • Mechanical Engineering

Keywords

  • Age hardenable Al alloys
  • Aircraft materials
  • Engineering correlations
  • Overaging
  • Thermal exposure

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