Fatigue Damage Mechanism of Titanium in Vacuum and in Air
Author:
Publisher
Elsevier BV
Subject
Applied Mathematics
Reference20 articles.
1. Wanhill, R.J.M., 1975. Fractography of Fatigue Crack Propagation in 2024-T3 and 7075-T6 Aluminum Alloys in Air and Vacuum, Metallurgical Transactions 6A, p. 1587.
2. Pelloux, R.J.N., 1969. Corrosion-fatigue Crack Propagation in “Fracture 1969” P.L. Pratt, Editor. Chapman & Hall, London, p. 731.
3. Alekseev, A.I., 1981. Slip Character and Fatigue Life of Copper Single Crystals in Air and in Vacuum, International Journal of Fatigue 3, p. 129.
4. Ranganathan, N., Petit, J., 1983. Quantitative Measurements in the Plastic Zone caused by a Single Overload in Air and Vacuum, in “Fatigue Mechanisms: Advances in Quantitative Measurement of Physical Damage, ASTM STP 811” American Society for Testing and Materials, Philadelphia, p. 464.
5. Snowden, K.U., 1964. The Effect of Atmosphere on the Fatigue of Lead, Acta Metallurgica 12, p. 295.
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