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Fatigue behavior of aluminum in vacuum.

NASA NTRS · Reprint (Version printed in journal) · 19670031324 · Published 2019-06-14 · Legacy CDMS · 1 author

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Abstract and citation only, verbatim from NASA NTRS; full text lives there. All credit to the authors and Legacy CDMS.

Abstract

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 ↗