Fatigue crack growth behaviour of Ti6Al4V at elevated temperature in high vacuum
Author:
Publisher
Elsevier BV
Subject
General Engineering
Reference8 articles.
1. The effect of stress ratio on the near-threshold fatigue crack growth behavior of Ti-8A1-1Mo-1V at elevated temperature
2. A comparison of test methods for the determination of fatigue crack growth rate threshold in titanium at elevated temperature
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4. Fatigue Crack Growth Threshold Concepts;Gerdes,1983
5. Proceedings of Short Fatigue Crack Conference;Petit,1990
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1. Numerical modeling of heat conduction in bodies with cracks;Acta Astronautica;2024-01
2. Effects of Temperature and Stress Ratio on Stage II Fatigue Crack Propagation in Bimodal Ti–6Al–4V;MATERIALS TRANSACTIONS;2021-07-01
3. FATIGUE CRACK GROWTH IN TWO ADVANCED TITANIUM ALLOYS UNDER CONSTANT AND VARIABLE AMPLITUDE LOADING AT 25 AND 175 °C;Fatigue & Fracture of Engineering Materials & Structures;2002-04-19
4. Fatigue Crack Growth of β-21S Titanium Alloy Under Constant Amplitude and miniTWIST Flight Spectra at 25°C and 175°C;Journal of Engineering Materials and Technology;1997-10-01
5. Fusion zone microstructure and fatigue crack growth behaviour in Ti-6Al-4V alloy weldments;Materials Science and Technology;1997-06
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