In support of Douglas Aircraft Co. structural damage tolerance analysis, crack propagation rates were measured in humid air from lo-\* to 10m3 mm/cycle of several high strength martensitic steels at stress ratios of R = 0.1 and R = 0.5. Increasing the stress ratio was found to decrease the threshold
β¦ LIBER β¦
Near threshold fatigue crack propagation behaviour of CrMoV turbine steel
β Scribed by J.H. Bulloch
- Publisher
- Elsevier Science
- Year
- 1995
- Tongue
- English
- Weight
- 773 KB
- Volume
- 23
- Category
- Article
- ISSN
- 0167-8442
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