Crack path in aeronautical titanium alloy under ultrasonic torsion loading

Crack path in aeronautical titanium alloy under ultrasonic torsion loading

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This paper discusses features of fatigue crack initiation and growth in aeronautical VT3-1 titanium alloy under pure torsion loading in gigacycle regime. Two materials: extruded and forged VT3-1 titanium alloys were studied. Torsion fatigue tests were performed up to fatigue life of 109 cycles. The...

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Bibliographic Details
Main Authors:	A. Nikitin, C. Bathias, T. Palin-Luc, A. Shanyavskiy
Format:	Article
Language:	English
Published:	Gruppo Italiano Frattura 2015-12-01
Series:	Frattura ed Integrità Strutturale
Subjects:	Very-High Cycle Fatigue Titanium alloy Ultrasonic Crack growth
Online Access:	https://www.fracturae.com/index.php/fis/article/view/1646

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