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Effect of low temperature on fatigue and fracture properties of Ti-5Al-2.5Sn(ELI) for use in engine components

Authors :
Ryder, J. T
Witzell, W. E
Publication Year :
1985
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1985.

Abstract

Experiments were conducted to evaluate the characteristics of the Ti-5Al-2.5Sn (ELI) alloy used in a fuel pump impeller at cryogenic temperatures. Tension, fracture toughness, and fatigue crack propagation data were collected determining the effect of frequency and load ratio on crack propagation. The results revealed that tensile strength increased significantly at 20 K compared to room temperature and fracture toughness was reduced at cryogenic temperatures. The fatigue crack growth rate was not sensitive to experimental conditions and there were only minimal crack orientation effects. Different frequencies produced no effect. At various temperatures and frequencies a load ratio increase resulted in higher crack growth rates. At low stress intensity levels the fatigue rate for both temperatures was the same; however, at high stress intensity levels the crack growth rate at 20 K increased because of the decrease in fracture toughness. The results correlated well with previous data.

Subjects

Subjects :
Metallic Materials

Details

Language :
English
Database :
NASA Technical Reports
Notes :
NAS3-18896
Publication Type :
Report
Accession number :
edsnas.19850065821
Document Type :
Report