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

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©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

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