Comparison and Evaluation of Low-Cycle Fatigue Life Prediction Methods Using Cu-Cr Alloy Developed for Rocket Engines

Author:

Park Jongchan,Kim Jae-Hoon,Lee Keum-Oh

Publisher

The Korean Society of Propulsion Engineers

Subject

General Medicine

Reference23 articles.

1. “Chromium Copper”, retrieved 26 Mar. 2021 from http://www.copper.org/resources/properties/microstructure/chrom_cu.html.

2. Lee, K.O., Rye, C.S., Heo, S.C. and Choi, H.S., “A Study on Strength Improvement of Copper Alloy for Combustion Chamber of Liquid­Propellant Engine,” 2013 KSPE Fall Conference, Gyeongju, Korea, pp. 328-331, 2013.

3. Conway, J.B., Stentz, R.H. and Berling, J.T., “High Temperature, Low­Cycle Fatigue of Copper­Base Alloys in Argon; Part IPreliminary Results for 12 Alloys at 1000℉(538℃),“ NASA CR­121259, 1973.

4. Ellis, L.D., “Observations of a Cast Cu­Cr­Zr Alloy,” NASA/TM­2006­213968, 2006.

5. Low Cycle Fatigue Behaviour of a Cu-Cr-Zr-Ti Alloy

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