Effect of Strengthened Hole on the Fatigue Life of 7050-T7451 Double-Shear Joints
Congress, AeroTech ; 2013 ; Montreal, Canada
2013-01-01
2311 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Effect of Strengthened Hole on the Fatigue Life of 7050-T7451 Double-Shear Joints
SAE Technical Papers | 2013
|Fatigue life prediction for 7050-T7451 aluminum alloy plate with scratch defect
British Library Online Contents | 2015
|Fatigue and Crack Growth in 7050-T7451 Aluminum Alloy Under Constant- and Variable-Amplitude Loading
Online Contents | 2013
|