The influence of burr formation and feed rate on the fatigue life of drilled titanium and aluminium alloys used in aircraft manufacture

Author:

Abdelhafeez Ali M.,Soo Sein Leung,Aspinwall David K.,Dowson Anthony,Arnold Dick

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering

Reference29 articles.

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2. Development of Single Step Drilling Technology for Multilayer Metallic-Composite Stacks using Uncoated and PVD Coated Carbide Tools;Kuo;Journal of Manufacturing Processes,2018

3. The Effect of Hole Quality on the Fatigue Life of 2024-T3 Aluminum Alloy Sheet. NASA/TM-2004-212658 ARL-TR-3106;Everett,2004

4. Fatigue Performance of Production-Quality Aircraft Fastener Holes;Ralph;International Journal of Fatigue,2007

5. Assessment of Residual Stresses and Hole Quality on the Fatigue Behavior of Aircraft Structural Joints – Volume 1: Stress Analyses, Fatigue Tests, and Life Predictions Technical Report DOT/FAA/AR-07/56,V1;Newman,2009

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