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NASA NTRS · Conference Paper

Fatigue behavior of aluminum and titanium sheet materials down to -423 deg f.

Published 2019-05-23 From Legacy CDMS 3 authors
View on NASA NTRS ↗

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.

Tension-compression fatigue properties under axial loading for aluminum and titanium sheet metal

Authors

  • Keys, R. D.
  • Kiefer, T. F.
  • Schwartzberg, F. R.

Keywords

  • CRYOGENICS
  • FATIGUE TEST
  • AXIAL LOAD
  • SHEET METAL
  • TITANIUM ALLOY
  • ALUMINUM ALLOY
  • STRUCTURAL MATERIAL

Citation: Keys, R. D., Kiefer, T. F., Schwartzberg, F. R. (2019). Fatigue behavior of aluminum and titanium sheet materials down to -423 deg f.. Legacy CDMS. NASA NTRS ID 19650049380. https://ntrs.nasa.gov/citations/19650049380 ↗