The influence of high temperature exposure on the mechanical performance of a γ titanium aluminide alloy

Materials Science and Engineering: A

Volumn 325, Issue 1-2, 2002, Pages 270-280

  Planck, S K ^a   Rosenberger, A H ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Fatigue; High temperature embrittlement; Strength; titanium aluminide

Indexed keywords

CRACK PROPAGATION; DUCTILITY; FATIGUE OF MATERIALS; HIGH TEMPERATURE EFFECTS; STRENGTH OF MATERIALS; TENSILE PROPERTIES;

SURFACE LAYER;

TITANIUM ALLOYS;

EMBRITTLEMENT; FATIGUE; HIGH TEMPERATURE APPLICATION; STRENGTH ASSESSMENT; TITANIUM ALLOY;

EID: 0037186701     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0921-5093(01)01470-8     Document Type: Article

References (26)

1. Reliability issues affecting the implementation of gamma titanium aluminides in turbine engine applications
2. An overview of the structural capability of available gamma titanium aluminide alloys
3. The effects of prolonged high temperature air exposure on the monotonic and cyclic properties of a gamma titanium aluminide alloy
4. Scale-up of ingot metallurgy wrought γ-TiAl
5. Isothermal and cyclic oxidation behavior of titanium aluminides
6. Specimen temperature measurement using looped-wire thermocouples
7. A rapid method for generation of a haigh diagram for high cycle fatigue
8. Aircraft engine applications for gamma titanium aluminide
9. Effects of microstructure, temperature, and environment on fatigue crack growth in Ti-46.5Al-3Nb-2Cr-0.2W γ titanium aluminide