Fatigue crack initiation and propagation in several nickel-base superalloys at 650°C
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Research context
OpenAlex topics: High Temperature Alloys and Creep · Fatigue and fracture mechanics · Nuclear Materials and Properties
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References (12)
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1. Cyclic behaviour of turbine disk alloys at 650°C10.1115/1.3224824 ↗
2. Evaluation of aircraft turbine disk alloys
3. Evaluation of cyclic behaviour of aircraft turbine disk alloys
4. Miner, R.V., Gayda, J. and Maier, R.D.Metall Trans (to be published)
5. The fracture morphology of nickel-base superalloys tested in fatigue and creep-fatigue at 650°C
6. High temperature crack growth structure-property relationships in nickel base superalloys
7. Micromechanisms of low-cycle fatigue in nickel-base superalloys at elevated temperatures
8. MATE: Quarterly progress report project 2
9. The effect of defects on the fatigue crack initiation process in two P/M superalloys: Part II. Surface — subsurface transition10.1007/BF02642414 ↗
10. Tada · 1973 · 10
11. The effect of ceramic inclusions on the low cycle fatigue life of low carbon Astroloy subjected to hot isostatic pressing10.1016/0025-5416(81)90004-5 ↗
12. Creep-fatigue-environment interactions in Astroloy