Cyclic crack growth behaviour of two nickel base turbine disc alloys

Date

1998-05-15

Author

Arslan, G
Doruk, M

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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.

Subject Keywords

Temperature

URI

https://hdl.handle.net/11511/65471

Journal

JOURNAL OF MATERIALS SCIENCE

DOI

https://doi.org/10.1023/a:1004369622557

Collections

Department of Metallurgical and Materials Engineering, Article

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.