Fatigue crack growth retardation after single-cycle peak overload in Ti-6Al-4V titanium alloy-Reference-Cited by-同舟云学术

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Fatigue crack growth retardation after single-cycle peak overload in Ti-6Al-4V titanium alloy

Published:1973-09 Issue:3 Volume:5 Page:585-604
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Jones R.E.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference13 articles.

1. A critical analysis of crack propagation laws;Paris;J. bas. Engng,1963

2. Numerical analysis of crack propagation in cyclic-loaded structures;Forman,1966

3. The effect of ground-to-air-cycles on the fatigue crack propagation in 2024-T3 alclad sheet material;Schijve;NLR, TRM. 2148,1966

4. On the Sharpness of Cracks Compared with Wells' COD;Srawley;NASA TMX-52904,1970

5. Fatigue crack closure under cyclic tension;Elber;Engng Fracture Mech.,1970

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1. A prediction method for new titanium alloy welded structure fatigue crack growth rate;Ships and Offshore Structures;2024-09-13

2. Experimental and analytical ways of finding the function of the maximum accumulated damage under operating modes with overloads;Advances in Industrial and Manufacturing Engineering;2024-05

3. Surface crack analysis of 8Cr4Mo4V steel based on Crystal/Phase microstructure model by grinding;Journal of Manufacturing Processes;2024-01

4. Effect of Uniaxial Pre-strain on Tensile, Work Hardening, Fracture Toughness, and Fatigue Crack Growth Rate of Titanium Alloy Ti–6Al–4V;Metallurgical and Materials Transactions A;2023-07-06

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