Cyclic crack growth behaviour of two nickel base turbine disc alloys

1998-05-15
Arslan, G
Doruk, M
The high temperature fatigue crack growth behaviour of the nickel base superalloys Alloy 718 and Rene 95 (specimen thickness = 4.1 mm) were investigated and compared with each other. Fatigue crack propagation (FCP) tests were carried out in laboratory air at room temperature and 600 degrees C by using C-T (compact tension) type specimen that were fatigue precracked at room temperature.

Citation Formats
G. Arslan and M. Doruk, “Cyclic crack growth behaviour of two nickel base turbine disc alloys,” JOURNAL OF MATERIALS SCIENCE, vol. 33, no. 10, pp. 2653–2658, 1998, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/65471.