Author:
Xie Yadan,Liu Keman,Zhao Jianjiang,Wei Hua
Publisher
Springer Science and Business Media LLC
Reference47 articles.
1. M. Courtis, C. Skamniotis, A. Cocks, and P. Ireland, Coupled Aerothermal-Mechanical Analysis in Single Crystal Double Wall Transpiration Cooled Gas Turbine Blades With a Large Film Hole Density, Appl. Therm. Eng., 2023, 219, p 119329.
2. G. Duscher, M.F. Chisholm, U. Alber, and M. Ruhle, Bismuth-Induced Embrittlement of Copper Grain Boundaries, Nat. Mater., 2004, 3, p 621–626.
3. M.R. Chellali, L. Zheng, R. Schlesiger, B. Bakhti, A. Hamou, J. Janovec, and G. Schmitz, Grain Boundary Segregation in Binary Nickel-Bismuth Alloy, Acta Mater., 2016, 103, p 754–760.
4. K. Harris, G.L. Erickson, S.L. Sikkenga, W.D. Brentnall, J.M. Aurrecoechea, and K.G. Kubarych, Development of Two Rhenium- Containing Superalloys for Single—Crystal Blade and Directionally Solidified Vane Applications in Advanced Turbine Engines, J. Mater. Eng. Perform., 1993, 2(4), p 481–487.
5. C. Fu, Y. Chen, S. He, S. Antonov, L. Li, W. Zheng, and Q. Feng, ICME Framework for Damage Assessment and Remaining Creep Life Prediction of in-Service Turbine Blades Manufactured with Ni-based Superalloys, Integrating Materials and Manufacturing, Innovation, 2019, 8, p 509–520.