Plastic flow behavior of a Ti-Al-Nb-Mn alloy at high temperatures
Creators
Description
High-temperature deformation of a gamma TiAl-based alloy containing 49.5 pct Al, 2.5 pct Nb and 1.1 pct Mn is studied using the constant-strain-rate isothermal compression-test technique. Axisymmetric tests were conducted in the strain rate range 0.001 to 10.0/s and at temperatures ranging from 1000 to 1400 C. The flow curves obtained at temperatures below 1250 C exhibit significant flow softening. This is correlated with the occurrence of shear localization, dynamic recrystallization, and wedge cracking. The flow-stress data are analyzed in terms of the strain-rate and temperature sensitivity. Strain-rate sensitivity decreases continuously with an increase in the strain rate and a decrease in the test temperature. In contrast, temperature sensitivity decreases with an increase in strain rate at all temperatures above 1050 C. A constitutive relationship between flow stress and the temperature-compensated strain rate is found to be valid in the temperature range 1000-1250 C. 20 refs
Additional details
Publishing Information
- Publisher
- Minerals, Metals, and Materials Society.
- Imprint Place
- Warrendale, PA (United States)
- Imprint Title
- Microstructure/property relationships in titanium aluminides and alloys; Proceedings of the Symposium, Fall Meeting of the Minerals, Metals, and Materials Society, Detroit, MI, Oct. 7-11, 1990
- Imprint Pagination
- 684 p.
- Journal Page Range
- p. 237-251.
Conference
- Title
- Fall meeting of the Minerals, Metals and Materials Society (TMS).
- Dates
- 7-11 Oct 1990.
- Place
- Detroit, MI (United States).
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 23070023
- Subject category
- S36: MATERIALS SCIENCE;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- ALUMINIUM ALLOYS; DEFORMATION; INTERMETALLIC COMPOUNDS; MANGANESE ALLOYS; NIOBIUM ALLOYS; PLASTICITY; RECRYSTALLIZATION; SHEAR; STRAIN RATE; TEMPERATURE DEPENDENCE; TEMPERATURE RANGE 1000-4000 K; THERMAL STRESSES; TITANIUM ALLOYS
- Descriptors DEC
- ALLOYS; MECHANICAL PROPERTIES; STRESSES; TEMPERATURE RANGE
Optional Information
- Secondary number(s)
- CONF-901008--.