Journal
INTERNATIONAL JOURNAL OF FATIGUE
Volume 138, Issue -, Pages -Publisher
ELSEVIER SCI LTD
DOI: 10.1016/j.ijfatigue.2020.105649
Keywords
Thermomechanical fatigue/cycling; Aerospace; Plasticity; Corrosion fatigue; Copper alloys
Funding
- German Research Foundation (Deutsche Forschungsgemeinschaft - DFG) [Sonderforschungsbereich Transregio 40]
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A detailed knowledge of the life-limiting mechanisms of regeneratively cooled rocket combustion chambers is important to increase the safety, the thrust-to-weight ratio and the cost-efficiency of future rocket engines. For this purpose, an actively cooled specimen made of CuCr1Zr is mounted downstream of a combustion chamber. The specimen is loaded cyclically and inspected after each cycle. The specimens collapse in the 'doghouse' failure mode after several load cycles. The effects of different hot-gas and coolant conditions, surface roughness and thermal barrier coatings on the lifetime are studied. The life-limiting mechanisms: creeping, yielding, abrasion, blanching and thermal aging are discussed.
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