Advertisement

Practical Failure Analysis

, Volume 1, Issue 4, pp 70–72 | Cite as

Response to comments on ‘effect of prior processing on the performance of PH 13-8 Mo stainless steel helicopter components’

  • M. S. Pepi
  • S. M. Grendahl
  • V. K. Champagne
Communications
  • 48 Downloads

Conclusion

The conclusions drawn for this investigation seemed appropriate from the results obtained. It is true that machining may have played a role in the components tested at AATD, but ARL does not feel this was the root cause of the premature “C” rod failures.

Keywords

Fatigue Material Specimen Practical Failure Analysis Volume Tool Mark Thread Root 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

Copyright information

© ASM International - The Materials Information Society 2001

Authors and Affiliations

  • M. S. Pepi
    • 1
  • S. M. Grendahl
    • 1
  • V. K. Champagne
    • 1
  1. 1.U.S. Army Research LaboratoryWeapons and Materials Research DirectorateAberdeen Proving Ground

Personalised recommendations