Failure Analysis of a Shot-Peened Component

730579

02/01/1973

Event
National Automobile Engineering Meeting
Authors Abstract
Content
A comprehensive scanning electron microscope(SEM) survey of the fracture surfaces of an aircraft main landing gear shock strut piston showed that improper shot peening contributed to the initiation of the anamolous fatigue failure.
SEM photographs of the suspect-origin regions and the surrounding areas were analyzed. The photographs are presented, along with a detailed description of the regions observed. Failure mechanism is discussed, and causes of fracture origin explored.
Meta TagsDetails
DOI
https://doi.org/10.4271/730579
Pages
12
Citation
Johari, O., and Sipes, W., "Failure Analysis of a Shot-Peened Component," SAE Technical Paper 730579, 1973, https://doi.org/10.4271/730579.
Additional Details
Publisher
Published
Feb 1, 1973
Product Code
730579
Content Type
Technical Paper
Language
English