FATIGUE CRACK GROWTH IN NICKEL‐BASED SUPERALLOYS AT 500‐700°C. II: DIRECT‐AGED ALLOY 718
- 1 March 1994
- journal article
- Published by Wiley in Fatigue & Fracture of Engineering Materials & Structures
- Vol. 17 (3) , 313-325
- https://doi.org/10.1111/j.1460-2695.1994.tb00232.x
Abstract
No abstract availableKeywords
This publication has 15 references indexed in Scilit:
- Depth of intergranular oxygen diffusion during environment-dependent fatigue crack growth in alloy 718Materials Science and Engineering: A, 1992
- Fatigue Crack Propagation in Alloy 718: A ReviewPublished by The Minerals, Metals and Materials Society ,1989
- The Development of Direct Age 718 for Gas Turbine Engine Disk ApplicationsPublished by The Minerals, Metals and Materials Society ,1989
- Effect of Frequency on Fatigue Crack Growth Rate of Inconel 718 at High TemperaturePublished by ASTM International ,1988
- Microstructural characterization and elemental partitioning in a direct-aged superalloy (DA 718)Materials Science and Engineering, 1987
- The effect of grain size upon the fatigue-crack propagation behavior of alloy 718 under hold-time cycling at elevated temperatureEngineering Fracture Mechanics, 1986
- A Model for Creep/Fatigue Interactions in Alloy 718Published by ASTM International ,1985
- The effect of microstructure and environment on the crack growth behaviour of Inconel 718 alloy at 650 °C under fatigue, creep and combined loadingMaterials Science and Engineering, 1982
- Effects of Stress Ratio and Hold-Time on Fatigue Crack Growth in Alloy 718Journal of Engineering Materials and Technology, 1979
- Frequency and wave-form effects on the fatigue crack growth behavior of alloy 718 at 298 K and 823 KMetallurgical Transactions A, 1978