Fatigue behavior of aluminum in vacuum.

Published 2019-06-14 From Legacy CDMS 1 author

Attribution

This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

Tenfold increase in fatigue life of 1100 aluminum in reverse bending at vacuum level below 10-2 torr due to retardation of crack propagation phase of fatigue process

Author

Hordon, M. J.

Keywords

CRACK PROPAGATION
ALUMINUM
FATIGUE LIFE
BENDING FATIGUE

Citation: Hordon, M. J. (2019). Fatigue behavior of aluminum in vacuum.. Legacy CDMS. NASA NTRS ID 19670031324. https://ntrs.nasa.gov/citations/19670031324 ↗