The Materials Systems Laboratory at the Massachusetts Institute of Tec
hnology has conducted research to develop decision tools that can faci
litate materials selection and provide a deeper understanding of the d
esign tradeoffs that occur when choosing among advanced aerospace mate
rials for high-temperature applications. As an illustration of the use
of these tools, this paper describes research done to evaluate the ma
terial alternatives currently under consideration for exhaust ducts in
aircraft gas turbine engines. Although nickel-based superalloys curre
ntly prevail for this application, the increasing temperatures of mode
rn engines are necessitating the usage of higher temperature materials
.