Parametric study to mitigate fretting fatigue in dovetail joint of aeroengine compressor
Fretting fatigue is most likely to occur in the dovetail joint of aero engine compressor resulting in small amplitude displacement of a few micrometers. This leads to degradation of the material in the form of fatigue strength and corrosion. This paper reports optimal conditions of blade geometrical...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
JVE International
2017-03-01
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| Series: | Journal of Measurements in Engineering |
| Subjects: | |
| Online Access: | https://www.jvejournals.com/article/18270 |