SPONSORING / MONITORING AGENCY NAME(S) AND ADDRESS(ES)Air Force
SPONSOR/MONITOR'S ACRONYM{S)APOSR/NL
SPONSOR/MONITOR'S REPORT NUMBER(S)13. SUPPLEMENTARY NOTES 14. ABSTRACT Prevention or at least delay of thermal barrier coating failure is the main objective of this research, in order to increase the service lifetimes of aircraft engines. To this end, it is critical to first understand mechanisms of failure, and then use that insight to design materials countermeasures. This grant supported the following research efforts in those directions:• Developments of a new pseudopotential theory and a solid state transition path search algorithm.• Applications of first principles density functional theory to:• metal-ceramic, silicon-ceramic, and ceramic-ceramic interfaces • dopants placed between alumina and late transition metals, with implications for catalysis • fatigue in silicon and alumina • temperature hysteresis in the monoclinic-to-tetragonal phase transformation pathway for zirconia • dopants and impurities on a NiAl alloy • understanding the stability of early-late transition metal intermetallics Metal jet turbine engine components are protected by a multilayer, multi-component material known as a thermal barrier coating (TBC), comprised of a NiAl-based "bond