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Acoustic emission tracks aircraft structure fatigue

โœ Scribed by CISE

Book ID
103539499
Publisher
Elsevier Science
Year
1987
Tongue
English
Weight
276 KB
Volume
9
Category
Article
ISSN
0142-1123

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Acoustic emission was obtained during fatigue crack propagation in a D6 tool steel and a 1015 mild steel using two different load ratios, R. It was found that the slope of the acoustic emission count rate vs stress intensity factor was higher when R = 0.2 than when R = 0.4. These results are describ