## Abstract High temperature fatigue in nickel‐base superalloys for aero‐engine applications requires consideration of cycle‐ and time‐dependent phenomena. For waveforms with dwells and/or low frequencies crack growth rates may be significantly accelerated up to the point of fully time‐dependent cr
Effect of hold time and environment on Fatigue Crack Growth Rate in Ti Alloys
✍ Scribed by Dr. D. Munz; V. Bachmann
- Publisher
- John Wiley and Sons
- Year
- 1980
- Tongue
- English
- Weight
- 491 KB
- Volume
- 11
- Category
- Article
- ISSN
- 0933-5137
No coin nor oath required. For personal study only.
✦ Synopsis
Abstract
In titanium alloys an effect of hold time at maximum load in a cyclic test is observed if K~max~ exceeds the threshold for crack propagation at a constant load test. For tests in air it is possible to predict crack growth rate for a hold time cycle from the crack growth rates from a cyclic test with triangular wave form and a constant load test. In 3.5% NaCl solution the measured crack growth rate is lower than the predicted.
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