TY - JOUR
T1 - 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
AU - Jabra, J.
AU - Romios, M.
AU - Lai, J.
AU - Lee, E.
AU - Setiawan, M.
AU - Lee, E. W.
AU - Witters, J.
AU - Abourialy, N.
AU - Ogren, J. R.
AU - Clark, R.
AU - Oppenheim, T.
AU - Frazier, W. E.
AU - Es-Said, O. S.
PY - 2006/10
Y1 - 2006/10
N2 - 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.
AB - 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.
KW - Age hardenable Al alloys
KW - Aircraft materials
KW - Engineering correlations
KW - Overaging
KW - Thermal exposure
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U2 - 10.1361/105994906X136142
DO - 10.1361/105994906X136142
M3 - Article
AN - SCOPUS:33750216503
SN - 1059-9495
VL - 15
SP - 601
EP - 607
JO - Journal of Materials Engineering and Performance
JF - Journal of Materials Engineering and Performance
IS - 5
ER -