Journal Published Online: 01 September 1976
Volume 4, Issue 5

Elevated Temperature Fatigue of Aluminum Alloy 5454 [Addendum to “Low Cycle Fatigue of Aluminum Alloys”]

CODEN: JTEVAB

Abstract

Fatigue data for aluminum alloy 5454 in the annealed condition and in the half-hard and stabilized condition, at a test temperature of 300°F (149°C), are given. These data are developed from load-controlled tests and cover the cyclic life region from about 1 × 105 to 2 × 106. The data supplement previously presented data from strain-controlled tests covering the cyclic life region below 1 × 104 cycles.

Author Information

Brodrick, RF
Teledyne Materials Research, Waltham, Mass.
Pages: 3
Price: $25.00
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Stock #: JTE10526J
ISSN: 0090-3973
DOI: 10.1520/JTE10526J