FATIGUE CRACK GROWTH IN TWO ADVANCED TITANIUM ALLOYS UNDER CONSTANT AND VARIABLE AMPLITUDE LOADING AT 25 AND 175 °C
Author:
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1046/j.1460-2695.1998.00067.x/fullpdf
Reference28 articles.
1. JC Newman 1981 A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading In: Methods and Models for Predicting Fatigue Crack Growth under Random Loading
2. RI Stephens DK Chen BW Hom 1976 Fatigue crack growth with negative stress ratio following single overloads in 2024-T3 and 7075-T6 aluminum alloys Fatigue Crack Growth Under Spectrum Loads
3. Overload induced crack growth rate attenuation behavior in aluminum alloys;Vecchio;Scripta Metall.,1983
4. S Suresh AK Vasudevan 1983 Application of fatigue threshold concepts to variable amplitude crack propagation Fatigue Crack Growth Threshold Concepts
5. CM Ward-Close RO Ritchie 1988 On the role of crack closure mechanisms in influencing fatigue crack growth following tensile overloads in a titanium alloy: near threshold versus higher Δ K behavior Mechanics of Fatigue Crack Closure
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1. Damage accumulation modeling under uniaxial low cycle fatigue at elevated temperatures;Engineering Failure Analysis;2015-10
2. Influence of Microstructure and Stress Ratio on Fatigue Crack Growth in a Ti-6-22-22-S alloy;Materials Today: Proceedings;2015
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