Constant Amplitude and Post-Overload Fatigue Crack Growth Behavior in PM Aluminum Alloy AA 8009

Author(s)

Anthony P. Reynolds, University of South Carolina - ColumbiaFollow

Document Type

Article

Publication Info

Published in Fatigue & Fracture of Engineering Materials & Structures, Volume 15, Issue 6-7, 1992, pages 551-562.

Rights

©Fatigue & Fracture of Engineering Materials & Structures 1992, John Wiley & Sons.

Reynolds, A. P. (June 1992). Constant Amplitude and Post-Overload Fatigue Crack Growth Behavior in PM Aluminum Alloy AA 8009. Fatigue & Fracture of Engineering Materials & Structures, 15 (6), 551-562. http://dx.doi.org/10.1111/j.1460-2695.1992.tb01294.x